<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">WJM</journal-id><journal-title-group><journal-title>World Journal of Mechanics</journal-title></journal-title-group><issn pub-type="epub">2160-049X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjm.2013.32010</article-id><article-id pub-id-type="publisher-id">WJM-30867</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Development of Analytical Model for Modular Tank Vehicle Carrying Liquid Cargo
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>.</surname><given-names>Toumi</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>M.</surname><given-names>Bouazara</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>M.</surname><given-names>J. Richard</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mechanical Engineering, Laval University, Quebec, Canada</addr-line></aff><aff id="aff1"><addr-line>Department of Applied Sciences, University of Quebec at Chicoutimi, Saguenay, Canada</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>mbouazar@uqac.ca(MB)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>04</month><year>2013</year></pub-date><volume>03</volume><issue>02</issue><fpage>122</fpage><lpage>138</lpage><history><date date-type="received"><day>February</day>	<month>27,</month>	<year>2013</year></date><date date-type="rev-recd"><day>April</day>	<month>8,</month>	<year>2013</year>	</date><date date-type="accepted"><day>April</day>	<month>15,</month>	<year>2013</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   The study of dynamics of tank vehicles carrying liquid fuel cargo is complex. The forces and moments due to liquid sloshing create serious problems related to the instability of tank vehicles. In this paper, a complete analytical model of a modular tank vehicle has been developed. The model included all the vehicle systems and subsystems. Simulation results obtained using this model was compared with those obtained using the popular TruckSim software. The comparison proved the validity of the assumptions used in the analytical model and showed a good correlation under single or double lane change and turning manoeuvers. 
 
</p></abstract><kwd-group><kwd>Analytical Model; Tank Vehicle; Stability; Dynamic Behavior; Suspension</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>In general, numerical models are developed to understand the liquid sloshing phenomenon coupled with tank structure. They are able to determine the coupling behavior, only under specific conditions, such as periodic accelerations. The effects of suspension system, tire and road excitation on a moving vehicle have not been taken into consideration. Regarding the vehicle itself, different simple models for tractors and trailers have been described in literatures to study the dynamic behavior of heavy vehicles during various maneuvers. Ellis [<xref ref-type="bibr" rid="scirp.30867-ref1">1</xref>] developed a simple model for tractor-trailer type bicycle with four degrees of freedom where the load transfer was modeled using an additional degree of freedom (rolling motion). Hyun [<xref ref-type="bibr" rid="scirp.30867-ref2">2</xref>] adopted a model for vehicle with four degrees of freedom for the active control of roll-over of heavy vehicles. While various solid-liquid models have been developed to determine the dynamic behavior of vehicles carrying liquids, few models have been developed to reflect the effects of vehicle systems and subsystems, such as suspension and tire components. The models adopted for the vehicle systems are all based on simplified assumptions.</p><p>It is necessary to develop a comprehensive model because a vehicle is composed of various subsystems and the effects of those need to be considered. AutoSim package, one of most popular software for modeling of the behavior of a vehicle, was developed at the University of Michigan [3,4]. Three software applications were created based on the AutoSim package [<xref ref-type="bibr" rid="scirp.30867-ref5">5</xref>]. These software applications are CarSim, TruckSim and BikeSim for cars, heavy vehicles and motorcycles respectively. However, the TruckSim software does not include the effects of motion of a moving load [6-8]. They are easy to use for conventional vehicles only. However, they offer some models for unconventional designs and the models find applications in some specific research projects. Another drawback with these tools is that they work in a closed environment. Therefore the present work focussed on development of custom made models.</p></sec><sec id="s2"><title>2. Vehicle Kinematic</title><p>To develop the model of the vehicle, there are several methods that could be exploited to derive the equations of motion such as Lagrange, Newton and virtual work methods. The popular alternative approach for dynamic modelling of vehicles is to use of simple models having a reasonable excution time. In this study, a new model was developed based on the simplified Ervin model [<xref ref-type="bibr" rid="scirp.30867-ref4">4</xref>]. This model was solved without any mathematical approximation and it took care of the complexity of liquid motion inside the tank. The solutions of the equations were obtained using the mathematical software Maple [<xref ref-type="bibr" rid="scirp.30867-ref9">9</xref>]. The equations were derived based on the principles of Newtonian mechanics and conservation of linear and angular momentums for a solid body.</p><sec id="s2_1"><title>2.1. Coordinate System</title><p>The large number of degrees of freedom for translation and rotational motion, required to represent an articulated vehicle, excludes the use of a single coordinate system. In fact, the equations of motion can be written more easily if several coordinate systems are employed. The purpose of this section is to identify the orientation of the various coordinate systems, and specify the variables required to connect the processing unit vectors in the various systems. The inertial coordinate system, the body coordinate system fixed to the sprung mass and the coordinate system fixed to the unsprung mass were used to describe the system. Newton’s laws are valid only for a finite acceleration in an inertial coordinate system<img src="4-4900186\00316c73-963c-47fd-8f7e-7523ab4b823a.jpg" />. The orientations of coordinate axes were expressed in accordance with the Society of Automotive Engineers’ standard (SAE), where the positive x axis points anterior, the positive y axis is oriented to the right and the positive z axis points downward. In our model, each sprung mass was represented as a rigid body with six degrees of freedom namely, longitudinal, lateral, vertical, roll, pitch and yaw. For the unsprung mass, there were assigned two degrees of freedom namely, the roll and vertical motions relative to the point of attachment of the sprung mass. The equations were formulated such that there was no limit to the number of sprung and unsprung masses. All the equations were solved, without any mathematical simplification, using the symbolic computational software Maple [<xref ref-type="bibr" rid="scirp.30867-ref9">9</xref>].</p><p>Three coordinate systems were used to develop the equations of motion. The first one was attached to the inertial system<img src="4-4900186\e83a82f1-1500-44bc-8c93-a21b6733f533.jpg" />, the second one was attached to each sprung mass <img src="4-4900186\571b0e84-e8b0-4ede-a682-f00df7f02097.jpg" /> and the third one was attached to each unsprung mass<img src="4-4900186\254fdbb2-b18a-4f84-b877-0a83e7726121.jpg" />. <xref ref-type="fig" rid="fig1">Figure 1</xref></p><p>shows the coordinate systems for fixed unit and articulated vehicles.</p><sec id="s2_1_1"><title>2.1.1. Coordinate System Fixed to the Sprung Mass</title><p>The three rotational motions of the sprung mass were expressed by the three Euler angles: yaw <img src="4-4900186\6c74df2f-b9db-40b4-81ca-fae000d72a65.jpg" /> (around axis<img src="4-4900186\2f1b0857-0ef9-43b7-98a8-7302af6d6e1d.jpg" />), pitch <img src="4-4900186\44b7c29e-3248-4372-ba2d-c7d5e55592e5.jpg" /> (around axis<img src="4-4900186\19d58b1c-0342-4e5d-a4d8-a97c17e29713.jpg" />) and rolling motion <img src="4-4900186\f161cc9e-773d-4248-aff3-3e25b7854d67.jpg" /> (around axis<img src="4-4900186\23b887eb-80d4-4d95-a716-24aa440e6d6f.jpg" />) as shown by <xref ref-type="fig" rid="fig2">Figure 2</xref>.</p><p>The transformation matrix between inertial system and the system fixed to the sprung mass was defined separately for the three successive rotations: yaw, pitch and roll.</p><p>Yaw<img src="4-4900186\eab3042a-8872-4504-9a16-22afcb9d19f9.jpg" />:</p><p><img src="4-4900186\8bd9235b-da59-4e81-8b15-f6ba67569bc2.jpg" /></p><disp-formula id="scirp.30867-formula96462"><label>(1)</label><graphic position="anchor" xlink:href="4-4900186\db930e18-a3d0-48e6-bbcd-4596f372f92d.jpg"  xlink:type="simple"/></disp-formula><p>Pitch<img src="4-4900186\712e92c4-e4a0-471e-8b3c-a823270fb074.jpg" />:</p><disp-formula id="scirp.30867-formula96463"><label>(2)</label><graphic position="anchor" xlink:href="4-4900186\b37558fa-b360-4495-ad3f-d0e79528a88d.jpg"  xlink:type="simple"/></disp-formula><p>Roll<img src="4-4900186\5c2a9928-8ff0-4bc4-ba3d-62485a954268.jpg" />:</p><p><img src="4-4900186\8e4dc5a8-2e13-4c13-85ca-99d6772fe2da.jpg" /></p><disp-formula id="scirp.30867-formula96464"><label>(3)</label><graphic position="anchor" xlink:href="4-4900186\67be8ccc-9ef2-4613-9c6a-73f701a25ae1.jpg"  xlink:type="simple"/></disp-formula><p>The transformation matrix, connecting the inertial system and the system fixed to the sprung mass, was obtained by combining the three matrices as follows:</p><p><img src="4-4900186\0f2982bc-670e-48f7-9185-de52c0b83e85.jpg" /></p><disp-formula id="scirp.30867-formula96465"><label>(4)</label><graphic position="anchor" xlink:href="4-4900186\bfd64d5e-cde4-4bfa-973b-e2d984f2674c.jpg"  xlink:type="simple"/></disp-formula><p>where: (please see Equation (5) below)</p><p>and:</p><disp-formula id="scirp.30867-formula96466"><label>(6)</label><graphic position="anchor" xlink:href="4-4900186\46eaa48a-a08a-43e8-b86b-c67ec460251e.jpg"  xlink:type="simple"/></disp-formula><p>with index (<img src="4-4900186\eba886b0-9b94-4c54-82f5-488f81f8f035.jpg" />,<img src="4-4900186\09aba5b5-6af0-4fe6-b0ba-96645dba8a95.jpg" />).</p></sec><sec id="s2_1_2"><title>2.1.2. Linear and Angular Velocities of the Sprung Mass</title><p>The equations of motion of each sprung mass were developed and written for the system fixed to the sprung mass in terms of linear velocity <img src="4-4900186\ca4df3c9-444e-45de-992f-579eba211b8a.jpg" /> and angular velocity <img src="4-4900186\f8b89719-ac66-4c84-968f-84171225a5cc.jpg" /> of the center of mass of the sprung mass. In order to calculate the velocity and Euler angles, expressions connecting the linear and angular velocities for both the systems were developed.</p><disp-formula id="scirp.30867-formula96467"><label>(7)</label><graphic position="anchor" xlink:href="4-4900186\158dc880-50df-4342-9e00-a891c08dfa59.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96468"><label>(8)</label><graphic position="anchor" xlink:href="4-4900186\1375e9e7-04f1-464e-82d4-0b887c997ef5.jpg"  xlink:type="simple"/></disp-formula><p>Introducing the transformation matrices between the two systems, the relationship between the angular velocities can be calculated by the following equations:</p><p><img src="4-4900186\cf8fff0d-9222-4728-8986-4b0cb41e1f26.jpg" /></p><disp-formula id="scirp.30867-formula96469"><label>(9)</label><graphic position="anchor" xlink:href="4-4900186\bde7be36-2595-42e3-ad74-5a991a179caf.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\08790eb5-19cf-4638-b96d-c9a6171156d3.jpg" /></p></sec><sec id="s2_1_3"><title>2.1.3. Coordinate System Fixed to the Unsprung Mass</title><p>As mentioned earlier, two motions were assigned to each unsprung mass, namely, the roll motion and vertical motion relative to the sprung mass. It may be noted that the pitching motion of the unsprung mass, representing the axle of vehicle, is infinitely small and can be neglected [<xref ref-type="bibr" rid="scirp.30867-ref3">3</xref>]. The orientation of the sprung mass relative to the inertial coordinate system was defined by two rotational motions namely, yaw motion <img src="4-4900186\5444b443-b15c-4e10-9e73-b84bac00200e.jpg" /> and roll motion <img src="4-4900186\c3a4352a-afca-4ac8-b44f-867c943060c1.jpg" /> as illustrated in <xref ref-type="fig" rid="fig3">Figure 3</xref>.</p><p>The transformation matrix between the system fixed to the unsprung mass and the inertial system can be expressed as:</p><p>Yaw<img src="4-4900186\0703c1a6-b432-4a1d-a460-af850ebf9bfc.jpg" />:</p><p><img src="4-4900186\1ce3b3fd-8bb4-4898-bf89-c204edd751da.jpg" /></p><disp-formula id="scirp.30867-formula96470"><label>(10)</label><graphic position="anchor" xlink:href="4-4900186\b3e790c7-8c77-4c41-96cd-384eb624cce2.jpg"  xlink:type="simple"/></disp-formula><p>Roll<img src="4-4900186\1459d3b2-0c32-4e37-898d-5bd465ac9135.jpg" />:</p><p><img src="4-4900186\776b0743-3b0b-43e4-a113-ecab3fc587ac.jpg" /></p><disp-formula id="scirp.30867-formula96471"><label>(11)</label><graphic position="anchor" xlink:href="4-4900186\71bbde9d-e045-4728-912a-77074fe7d7fe.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96472"><label>(5)</label><graphic position="anchor" xlink:href="4-4900186\9ac78dd8-77f4-427b-94be-1f6a30e75d3d.jpg"  xlink:type="simple"/></disp-formula><p>&#160;</p><p>Therefore, the transformation matrix, that connects the system fixed to the unsprung mass and the inertial system, can be obtained by combining the above two transformations ((10) and (11)).</p><disp-formula id="scirp.30867-formula96473"><label>(12)</label><graphic position="anchor" xlink:href="4-4900186\11175efd-b2be-4651-ac23-b11ae9713656.jpg"  xlink:type="simple"/></disp-formula><p>The angular velocity of the unsprung mass can be defined by the following equation:</p><disp-formula id="scirp.30867-formula96474"><label>(13)</label><graphic position="anchor" xlink:href="4-4900186\bab73fe4-b185-4faf-a8bd-2a4dc779f5d1.jpg"  xlink:type="simple"/></disp-formula><p>By introducing the transformation matrices between the inertial system and the system fixed to the unsprung mass, the angular velocity was expressed in terms of Euler angles as follows:</p><disp-formula id="scirp.30867-formula96475"><label>(14)</label><graphic position="anchor" xlink:href="4-4900186\d227d88e-22ea-4851-ab6e-6a0dccfa65e7.jpg"  xlink:type="simple"/></disp-formula><p>On the other hand, the road excitation forces are in contact with the unsprung mass. These forces are transferred to the sprung mass through the suspension system. Therefore, the transformation matrix between the two systems fixed to the sprung and unsprung masses needs to be calculated.</p><disp-formula id="scirp.30867-formula96476"><label>(15)</label><graphic position="anchor" xlink:href="4-4900186\ec5a7d71-b6cf-40af-81b5-7ed2864e5a95.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96477"><label>(16)</label><graphic position="anchor" xlink:href="4-4900186\76cd386f-5ba1-4a13-b1a9-5097f899c3ed.jpg"  xlink:type="simple"/></disp-formula><p>where: (please see Equation (17) below).</p></sec></sec><sec id="s2_2"><title>2.2. Sprung Mass Kinematics</title><p>For the derivation of equations of motion of the vehicle it is necessary to calculate the expression for the acceleration of an arbitrary point on the vehicle. <xref ref-type="fig" rid="fig4">Figure 4</xref> shows <img src="4-4900186\a6bfb8ba-6f30-4c39-b360-b58267ab8183.jpg" /> as the coordinate system fixed to the road (inertial) and <img src="4-4900186\23c70396-132b-425f-9f68-0fcb43835356.jpg" />&#160;as the system of the body coordinate with a</p><p>translational velocity <img src="4-4900186\42383563-6494-418e-9400-e68ace7462e1.jpg" />&#160;and an angular velocity<img src="4-4900186\4dde5681-d0b8-4b03-905e-4455a5b60291.jpg" />. For a given vector<img src="4-4900186\3934cd79-a3be-4e4c-a18a-b02dd0f0a0a3.jpg" />, the following expression [<xref ref-type="bibr" rid="scirp.30867-ref10">10</xref>] was obtained:</p><disp-formula id="scirp.30867-formula96478"><label>(18)</label><graphic position="anchor" xlink:href="4-4900186\e35015df-ed32-441e-bffd-1d61be4801ad.jpg"  xlink:type="simple"/></disp-formula><p>The indices f and b indicate that the derivative was calculated with respect to the inertial system and system of the body concerned respectively.</p><p>The velocity of point p in the vehicle, relative to inertial system, can be calculated by the following expression:</p><disp-formula id="scirp.30867-formula96479"><label>(19)</label><graphic position="anchor" xlink:href="4-4900186\cf6817df-8738-4fa8-a03a-d166d1bdf7db.jpg"  xlink:type="simple"/></disp-formula><p>Therefore, substitution of Equation (18) in Equation (19) gives:</p><disp-formula id="scirp.30867-formula96480"><label>(20)</label><graphic position="anchor" xlink:href="4-4900186\ee2ecf29-3118-4515-b945-dc270bfdb1a2.jpg"  xlink:type="simple"/></disp-formula><p>The acceleration of the point <img src="4-4900186\8407fe0a-777b-472b-91f1-d93748c50406.jpg" /> can be calculated by differentiating Equation (20) with respect to time:</p><disp-formula id="scirp.30867-formula96481"><label>(21)</label><graphic position="anchor" xlink:href="4-4900186\ec83ca58-6513-4eee-a85c-d951fdb1aa23.jpg"  xlink:type="simple"/></disp-formula><p>Since the center of mass of the sprung mass coincides with the origin of the coordinate system attached to the sprung mass, acceleration of the center of mass of the sprung mass was obtained by replacing <img src="4-4900186\216452fa-4631-4171-89f3-580d59aad479.jpg" /> in Equation (21):<img src="4-4900186\608eac97-9d03-4cce-8e8f-a13ed47c63b9.jpg" />.</p><disp-formula id="scirp.30867-formula96482"><label>(22)</label><graphic position="anchor" xlink:href="4-4900186\0399f0c2-4bbf-4240-ab4b-dc4508b74cf2.jpg"  xlink:type="simple"/></disp-formula><p>In this study, it was assumed that the load of the liquid, represented by the center of mass, can move as a material point and can be represented by a remote vector <img src="4-4900186\406da7cb-06f4-4d04-8d88-344c0792900d.jpg" />&#160;from the center of mass of the sprung mass with the same angular velocity <img src="4-4900186\32046ff2-fecf-447a-a5d7-6dbbc8820cab.jpg" /> as that of the sprung mass of the vehicle as shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>.</p><disp-formula id="scirp.30867-formula96483"><label>(17)</label><graphic position="anchor" xlink:href="4-4900186\b4d69dd3-d6f5-4109-8956-d725bcd6eeff.jpg"  xlink:type="simple"/></disp-formula><p>Hence, the acceleration of the center of mass of the liquid can be obtained by replacing the expression <img src="4-4900186\832687f3-da97-44d1-9972-bc1a10031112.jpg" /> in Equation (21). Moreover, in this study the interaction between the vehicle and the liquid was modeled as a multi-body system using small time step<img src="4-4900186\89c75383-27da-4ae9-9d63-8659792af75e.jpg" />. As the coordinates of the vector <img src="4-4900186\976cf584-0cfd-47fa-aa77-939a65dfa30e.jpg" /> were updated at each time step, the relative velocity and acceleration relative to the coordinate system fixed to the sprung mass were neglected.</p><disp-formula id="scirp.30867-formula96484"><label>(23)</label><graphic position="anchor" xlink:href="4-4900186\69c15ad5-2e24-4b0b-9a58-f81a5d96cf44.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\1247d539-012e-461b-bf45-95e930336e28.jpg" /></p></sec><sec id="s2_3"><title>2.3. Unsprung Mass Kinematics</title><p>The position of the unsprung mass is located in relation to the point where the sprung mass is attached as shown in Figures 5 and 6.</p><disp-formula id="scirp.30867-formula96485"><label>(24)</label><graphic position="anchor" xlink:href="4-4900186\501e076c-e535-45a3-9040-024d45ac2d51.jpg"  xlink:type="simple"/></disp-formula><p>where:</p><p><img src="4-4900186\0f18da7d-0a9f-4201-8b98-0f8d5e843759.jpg" />: represents the position of center of sprung mass from the inertial system.</p><p><img src="4-4900186\233772bf-0801-41fa-abd5-cd1850eb6d1b.jpg" />: represents the position of the roll center relative to the system fixed to the sprung mass.</p><p><img src="4-4900186\5c101d1c-d998-4ff2-a150-3fa78af0e8c4.jpg" />: represents the position of the roll center relative to the system attached to the unsprung mass. The velocity was calculated by differentiating Equation (24) with respect to time:</p><disp-formula id="scirp.30867-formula96486"><label>(25)</label><graphic position="anchor" xlink:href="4-4900186\d0176373-3511-4b67-9158-be6fb56a3dab.jpg"  xlink:type="simple"/></disp-formula><p>The acceleration was calculated by differentiating Equation (25) with respect to time:</p><disp-formula id="scirp.30867-formula96487"><label>(26)</label><graphic position="anchor" xlink:href="4-4900186\be59268e-5876-4121-9cca-8ddd5f0f9bf3.jpg"  xlink:type="simple"/></disp-formula><p>where suffixes <img src="4-4900186\0fd0eecd-84f4-4c7b-891a-276b0c863fb7.jpg" /> and <img src="4-4900186\4cbbe105-da20-4b7e-afc3-ecbc78b0e092.jpg" /> indicate systems fixed to the sprung mass and unsprung mass respectively.</p><p><img src="4-4900186\11c619ff-862c-4e7f-a761-ff89304c4aa6.jpg" />is the angular velocity of the sprung mass and <img src="4-4900186\500cbf36-143b-4b5d-87d6-9c2f13c97723.jpg" /> is the angular velocity of the unsprung mass.</p><p>As described in <xref ref-type="fig" rid="fig7">Figure 7</xref>, suspension forces transmitted to the sprung mass for each axis can be expressed as follows:</p><disp-formula id="scirp.30867-formula96488"><label>(27)</label><graphic position="anchor" xlink:href="4-4900186\9fbecdec-daea-420b-b688-f93e67e9975b.jpg"  xlink:type="simple"/></disp-formula><p>where:</p><p><img src="4-4900186\78a6602f-b8d5-43da-ad9e-67b198d2dcde.jpg" />and <img src="4-4900186\84b71fae-6cb7-43c3-9bfb-0b6acf5a06b9.jpg" /> are the vertical suspension forces at left and right sides respectively.</p><p><img src="4-4900186\5fe9705b-db90-4a54-977c-31f7245998c8.jpg" />is the internal lateral force applied to the roll center of each axis. This force is the result of the lateral forces applied to the tires.</p><p><img src="4-4900186\868d1522-a021-482c-beda-9b6f5ecb0676.jpg" />and <img src="4-4900186\b481dbdf-6b35-4013-b5fb-2e7b2b812fc0.jpg" /> are the longitudinal suspension forces at the right and left sides respectively.</p><p>The suspension forces in the system attached to the sprung mass <img src="4-4900186\13f8f0b2-59b9-4f55-b57c-ac4f0562bd05.jpg" /> can be defined using the transformation matrix that connects the unsprung mass and sprung mass (Equation (17)).The internal forces can be eliminated according to the dynamic equations of motion for each axis<img src="4-4900186\15c1f705-0bd7-4f67-a207-521d8e12d368.jpg" />, as illustrated in <xref ref-type="fig" rid="fig7">Figure 7</xref>.</p><disp-formula id="scirp.30867-formula96489"><label>(28)</label><graphic position="anchor" xlink:href="4-4900186\fd5f84cf-85b6-494e-8522-67e80b6b343b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96490"><label>(29)</label><graphic position="anchor" xlink:href="4-4900186\9bf78c3c-441d-4449-9493-115e5e211195.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96491"><label>(30)</label><graphic position="anchor" xlink:href="4-4900186\062f45e1-93f3-4217-bc6c-6f4f52e90b61.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s2_4"><title>2.4. Fifth Wheel Kinematics</title><p>The motion of the sprung mass of tractor and trailer are coupled via the fifth wheel joint. Several studies suggested to consider joint connection as a rigid one in the case of translational motion. This allows to consider a joint as a point. With this assumption, the number of degrees of freedom was reduced. Thus we can calculate the expressions for velocity and acceleration of the trailer</p><p>depending on the velocity and acceleration of the tractor [<xref ref-type="bibr" rid="scirp.30867-ref4">4</xref>]. If the harness is not rigid enough, it can be modeled as an assembly of a spring and a damper in parallel [<xref ref-type="bibr" rid="scirp.30867-ref3">3</xref>]. However, torsional component of the fifth wheel acts in the case of rolling motion. From <xref ref-type="fig" rid="fig8">Figure 8</xref>, velocity and acceleration of point C were calculated with respect to the two systems fixed to the sprung masses of tractor and trailer as follows:</p><disp-formula id="scirp.30867-formula96492"><label>(31)</label><graphic position="anchor" xlink:href="4-4900186\2189a8b5-6cb3-4628-a42f-6e78a935d57c.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\13041a82-65a6-418a-8b36-700c905d3c17.jpg" /></p><p>with:</p><p><img src="4-4900186\cf5ba504-22bb-4d12-a503-706ec0867cc1.jpg" />and <img src="4-4900186\1ac6519b-a492-4dfc-99fe-bf4239e4c1e3.jpg" /></p><p>where:</p><p><img src="4-4900186\5dc5a96d-d790-409b-845b-0833c128d308.jpg" /></p><p><img src="4-4900186\1c23882f-e007-4f57-ad67-b2bc41213880.jpg" /></p><p>and</p><p><img src="4-4900186\127fb3d4-e8c6-45ea-8004-35620ce02e24.jpg" /></p><disp-formula id="scirp.30867-formula96493"><label>(32)</label><graphic position="anchor" xlink:href="4-4900186\54fde0ef-4dbc-45f2-84c2-dd04cd872b8b.jpg"  xlink:type="simple"/></disp-formula><p>The following relations can be obtained by introducing the expressions of Equation (32) in Equation (31).</p><disp-formula id="scirp.30867-formula96494"><label>(33)</label><graphic position="anchor" xlink:href="4-4900186\e975ab00-e605-4061-9da2-70f4c9be67af.jpg"  xlink:type="simple"/></disp-formula><p>The transformation matrix <img src="4-4900186\ea5c665f-1dd8-4040-b9fc-90570b3a730b.jpg" /> between the system attached to the sprung mass of trailer <img src="4-4900186\41246a2b-8d1e-4798-82d5-b2ecf6f3e7ec.jpg" /> and the system fixed to the sprung mass of tractor <img src="4-4900186\be024da8-2f3e-4f3f-a91b-f5e798afc0ed.jpg" /> can be calculated through the inertial system as follows:</p><p><img src="4-4900186\540a72e4-a9bd-409f-bcc0-187f373df4ba.jpg" />.</p><disp-formula id="scirp.30867-formula96495"><label>(34)</label><graphic position="anchor" xlink:href="4-4900186\de916209-fbc1-491e-8780-31d533ede032.jpg"  xlink:type="simple"/></disp-formula><p>The simultaneous solution of Equations (33) and (34) gave the final expressions for the velocity and acceleration of the trailer as a function of the velocity and acceleration of the tractor.</p><p>The sweep on the roll angle between the tractor and trailer was useful to calculate the constraint of the fifth wheel for the roll motion (roll moment):</p><p><img src="4-4900186\f3cf847b-30c6-48e0-91d3-2b0768213802.jpg" /></p><disp-formula id="scirp.30867-formula96496"><label>(35)</label><graphic position="anchor" xlink:href="4-4900186\14b8a8a0-ea4a-4a77-95e0-a80b96a85466.jpg"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s3"><title>3. Vehicle Kinetics</title><p>This section is devoted to the definition of variables with some algebraic manipulations chosen for the equations of motion. All kinetic parameters were developed for an articulated vehicle. The same settings were applied in the case of a unit vehicle. The free body diagram shown in <xref ref-type="fig" rid="fig7">Figure 7</xref> shows the external and internal forces and moments applied to each subsystem of the vehicle. To obtain the equations of linear and angular motions, it is important to model the rigid body as a set of material points.</p><sec id="s3_1"><title>3.1. Linear Motion</title><p>The application of Newton’s laws eventually gives the equations of linear motion for the tractor and trailer.</p><disp-formula id="scirp.30867-formula96497"><label>(36)</label><graphic position="anchor" xlink:href="4-4900186\0874d61c-1df5-489b-902c-bb8a23c67720.jpg"  xlink:type="simple"/></disp-formula><p>The equations of translational motion can be obtained by the combination of the Equations (36), (22), (24), (29), and (30). These equations were represented by second order differential equations for sprung mass si:</p><p><img src="4-4900186\eec247c2-7cb3-49a6-9391-15bd1a7346a9.jpg" /><img src="4-4900186\cce0306c-1cc2-4e97-93d5-d2eeeec470d5.jpg" /> (37)</p><p><img src="4-4900186\1d5fe4ff-8459-45f2-9fe6-d5c0d41bebb0.jpg" /><img src="4-4900186\e348efba-ba2e-4aa7-811d-ca86e350b3f5.jpg" /><img src="4-4900186\1014816d-ecd5-4143-b24f-ac5786e78322.jpg" /> (38)</p><disp-formula id="scirp.30867-formula96498"><label>(39)</label><graphic position="anchor" xlink:href="4-4900186\9126304d-8ba3-4df6-b9c8-cec66ca2f7b8.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="4-4900186\3389994a-77cb-4871-805b-503fc6d6133f.jpg" />: tractor</p><p><img src="4-4900186\f426c991-076a-4566-91a0-599da1243827.jpg" />: trailer.</p><p><img src="4-4900186\6fa1a779-f88f-4426-99f1-bc71b8eaba00.jpg" />: axle number.</p><p><img src="4-4900186\ea02d199-c14a-4859-b376-d9c2caecbc17.jpg" />: axle number. <img src="4-4900186\366b0b85-db8c-4fae-996b-f8f4ab7ae0b5.jpg" />for tractor and <img src="4-4900186\ce5f9455-af4d-497e-ae1b-0383bf753330.jpg" /> for trailer.</p><p><img src="4-4900186\78ba70d6-679c-40ee-b133-beded819b1e5.jpg" />: liquid.</p><p><img src="4-4900186\8ce27ded-3718-4494-8811-ff99dda12594.jpg" />: sprung mass<img src="4-4900186\a862ef31-84e7-43c3-8285-48fbcb00c127.jpg" />.</p><p>In this study the constraint forces due to the fifth wheel were eliminated by using the kinematic Equations (33) and (34) developed earlier. It should be noted that all these equations of motion were programmed in the Maple software in a systematic way. Therefore, to obtain the equations of motion in the case of a unit vehicle, only change of the indices <img src="4-4900186\085707a5-976d-440b-88d4-b7afc9648465.jpg" /> was needed.</p><p>The equation of vertical motion of the sprung mass for each axis <img src="4-4900186\e73aaaa2-ff4d-4aaa-a5e8-0666cb3e66d5.jpg" /> was given by the folowing expression:</p><disp-formula id="scirp.30867-formula96499"><label>(40)</label><graphic position="anchor" xlink:href="4-4900186\11ad61a0-a3aa-438d-8e9b-03ff93376f74.jpg"  xlink:type="simple"/></disp-formula><p>where:</p><p><img src="4-4900186\7a25683b-cfd5-47b6-823b-75e009f4c4e4.jpg" />: axle number.</p><p><img src="4-4900186\eeafb233-bcbe-4f78-8866-26fae60f3307.jpg" />: number of tires in each axle.</p><p><img src="4-4900186\108afaf5-6ad1-48af-bc45-f115ecebca31.jpg" />: <img src="4-4900186\df89dbe2-e7b5-40fc-9d9a-abb48de34e57.jpg" />fortractor front axle and <img src="4-4900186\98044b74-266c-47bd-954b-a010054036ea.jpg" /> for the other axles.</p></sec><sec id="s3_2"><title>3.2. Angular Motion</title><p>It is important to model the rigid body as a system of material points <img src="4-4900186\8a9a4d82-7f6f-4a7d-9bad-7358fe52412e.jpg" /> with masses <img src="4-4900186\93e53d5b-b00a-4b16-b244-6e52259bf404.jpg" /> to obtain the equation of angular motion. According to Newton’s equation, angular momentum relative to the inertial system can be given by the following expression:</p><disp-formula id="scirp.30867-formula96500"><label>(41)</label><graphic position="anchor" xlink:href="4-4900186\5735c109-d8f9-4fa9-ad7f-5a93e34f7bfb.jpg"  xlink:type="simple"/></disp-formula><p>Substituting Equation (21) in (41), the following expression can be obtained:</p><disp-formula id="scirp.30867-formula96501"><label>(42)</label><graphic position="anchor" xlink:href="4-4900186\ab31bcff-0dce-4bd3-9ac9-2be5835d0d60.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96502"><label>(43)</label><graphic position="anchor" xlink:href="4-4900186\2b83e0b7-06bc-455e-a5aa-c51323010618.jpg"  xlink:type="simple"/></disp-formula><p>The first term of Equation (43) can be simplified as:</p><p><img src="4-4900186\7251bd1c-d34e-434e-aa00-c8abe4162496.jpg" /></p><p>The second and third terms of Equation (43) can also be simplified [<xref ref-type="bibr" rid="scirp.30867-ref10">10</xref>] as:</p><p><img src="4-4900186\47af58b8-f37e-4ff0-984d-6018b82005f7.jpg" /></p><p><img src="4-4900186\0eede277-40f8-41e8-a95e-16fe109891de.jpg" /></p><p>Therefore Equation (42) takes the following form:</p><disp-formula id="scirp.30867-formula96503"><label>(44)</label><graphic position="anchor" xlink:href="4-4900186\2a7194d0-4bff-4997-9101-a8ead6fe24cf.jpg"  xlink:type="simple"/></disp-formula><p>Since the sprung mass center coincides with the origin of the body axis system<img src="4-4900186\ac88db4a-eb13-45a4-ab9a-249167c4cfe0.jpg" />, the expression of angular motion (44) can be formulated as follows:</p><disp-formula id="scirp.30867-formula96504"><label>(45)</label><graphic position="anchor" xlink:href="4-4900186\8e7d688e-0899-4d13-8786-241f24b490e8.jpg"  xlink:type="simple"/></disp-formula><p>The matrix of inertia <img src="4-4900186\6e668216-b4df-4b51-83be-8cc42e9fdcf2.jpg" /> was expressed in the system<img src="4-4900186\45ea428e-55fb-4fb6-9f84-f7ac6ac2e7e3.jpg" />as follows:</p><disp-formula id="scirp.30867-formula96505"><label>(46)</label><graphic position="anchor" xlink:href="4-4900186\5a421da5-476b-4459-8a19-1a81bdcd38c4.jpg"  xlink:type="simple"/></disp-formula><p>Since the tractor body and the trailer body can be modeled as contained bodies, all mathematical expressions can be expressed by integrals <img src="4-4900186\c008b75b-b941-4899-98fd-cca8082eb411.jpg" /> instead of a sums<img src="4-4900186\3212cb40-ffd6-4d4f-8375-5240e85046f7.jpg" />.</p><p>The moments applied to the sprung mass due to the liquid load and the suspension forces expressed in axis system fixed to the sprung mass were calculated as follows:</p><disp-formula id="scirp.30867-formula96506"><label>(47)</label><graphic position="anchor" xlink:href="4-4900186\dd0d5f62-473c-43e9-8b53-a5c94ef0bc96.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96507"><label>(48)</label><graphic position="anchor" xlink:href="4-4900186\dba7c2d2-7bd9-4a1a-be18-f59ea8a9cddd.jpg"  xlink:type="simple"/></disp-formula><p>Substituting in Equation (45), the terms of the moments due to the liquid charge (47), the moments of the suspension (48) and the moments due to the fifth wheel constraints (35), the final equations of angular motion of the sprung mass (si) can be obtained as follows:</p><p><img src="4-4900186\99583858-a307-46dd-a4d7-f05d70ac4bdc.jpg" /><img src="4-4900186\3a6b0263-326c-4ec3-9b4b-6af086a4d2ca.jpg" /><img src="4-4900186\b89c183f-c4e9-4981-b217-a7801079d3b4.jpg" /> (49)</p><disp-formula id="scirp.30867-formula96508"><label>(50)</label><graphic position="anchor" xlink:href="4-4900186\3b7d2841-eb02-4637-8420-b71ea290c9bc.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96509"><label>(51)</label><graphic position="anchor" xlink:href="4-4900186\570edb33-bc1a-4345-a811-f743dd01daa5.jpg"  xlink:type="simple"/></disp-formula><p>k: axle number k = 3 for tractor and k = 2 for trailer.</p><p>The equation for rolling motion of the sprung mass of each axle <img src="4-4900186\ba58add6-ead1-42df-b98b-92d08f7fd0af.jpg" /> can be given by the following expression:</p><disp-formula id="scirp.30867-formula96510"><label>(52)</label><graphic position="anchor" xlink:href="4-4900186\fe39f871-d725-4c60-8484-48b10cc0f369.jpg"  xlink:type="simple"/></disp-formula><p>where:</p><p><img src="4-4900186\b8468014-83eb-477d-a650-cc0bc7835575.jpg" />: axle index.</p><p><img src="4-4900186\f4f7cdb1-bc1e-4f24-a0ab-a984424bb9d2.jpg" />: number of tires in each axle.</p><p><img src="4-4900186\a7196a8f-ecbe-4924-b92e-d9e3c558d788.jpg" />: <img src="4-4900186\834d36a0-d222-4b45-a1e2-b43303950d2f.jpg" />for the front axle of the tractor and <img src="4-4900186\55068cea-cbd1-44cc-bac8-6de0f3e9f9c8.jpg" /> for other axles.</p></sec><sec id="s3_3"><title>3.3. Suspension Model</title><p>The external forces acting on the vehicle are generated mainly due to the contact forces between wheel and ground. These forces are transmitted to the sprung mass through the suspension system of the vehicle. To simplify the model, the suspension system was represented with a linear spring and a damper assembled in parallel. The vertical force applied on the vehicle through the suspension system was assumed to be equal to the sum of the static equilibrium force and the excitation forces.</p><disp-formula id="scirp.30867-formula96511"><label>(53)</label><graphic position="anchor" xlink:href="4-4900186\8e4626aa-bf83-41ed-87c1-43939009a282.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="4-4900186\f752cab4-ee44-4359-8263-4d89275bdcaa.jpg" /> is the suspension deflections and can be calculated based on the geometry of the vehicle.</p><p><img src="4-4900186\7cac8b5c-e3c7-4bd9-b8d7-a49c73157c69.jpg" /></p><disp-formula id="scirp.30867-formula96512"><label>(54)</label><graphic position="anchor" xlink:href="4-4900186\b0606a3a-b83b-4074-8174-fe588eb14306.jpg"  xlink:type="simple"/></disp-formula><p>where:</p><p><img src="4-4900186\602b1759-7dc5-448f-877f-891fc4001d61.jpg" />: sprung mass of tractor.</p><p><img src="4-4900186\ef8c4cba-5019-4731-b437-74617106caee.jpg" />: sprung mass of trailer.</p><p><img src="4-4900186\0e894e0e-03dc-4712-9391-bd8e91c47299.jpg" />: axle number (<img src="4-4900186\4dfd032e-4110-46bd-b818-94c9de1e477b.jpg" />for tractor and <img src="4-4900186\e427f531-7e26-4bfd-a215-ea001331f5c1.jpg" /> for trailer).</p></sec><sec id="s3_4"><title>3.4. Tire Model</title><p>The tire is an essential element in a vehicle. It represents the contact between wheel and ground. The forces and moments transmitted to the vehicle by the tires due to wheel-ground interaction are complex and nonlinear. These forces and moments depend primarily on normal forces, longitudinal and lateral load transfer, slip rate <img src="4-4900186\ecf048b9-9e59-4b33-b8b3-0c59aeac1bfb.jpg" /> and slip angles <img src="4-4900186\5b2c2417-9c48-4eda-a22f-ed32a8546f4b.jpg" /> as illustrated in <xref ref-type="fig" rid="fig9">Figure 9</xref>.</p><p>There are several models available for tires. Most studies have used linear model or models based on tables from experimental tests. The forces and moments were characterized according to vehicle velocity, normal force, longitudinal slip ratio and slip angle [4,11-14]. These models usually have a better prediction capability for the traction force of contact. However, their data are specific for the type of tire which reduces their universal use. There are other numerical models which use different analytical approaches [15-17]. The choice of model of</p><p>the tire affects the calculation of the efforts at the wheelsoil interface. The data from these models are important when one wants to make a dynamic model of a vehicle.</p><p>In this study the efforts of the tires were studied with the model called slip circle [11,18]. The model is closely related to the model of friction ellipse shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>0 [<xref ref-type="bibr" rid="scirp.30867-ref11">11</xref>].</p><p>With this model, it is possible to obtain lateral and longitudinal forces in the case of combined motions based only on measured data for separate motions such as, braking/traction alone or direction case, as illustrated in <xref ref-type="fig" rid="fig1">Figure 1</xref>1.</p><p>The calculation was based on the evaluation of friction <img src="4-4900186\a02837b1-8e37-44a7-b211-4989a3014069.jpg" />&#160;and<img src="4-4900186\856c1e07-2d03-4b15-90c8-608e33703ec8.jpg" />. The calculation of these coefficients depends on the rate of longitudinal slip <img src="4-4900186\3e22c417-63a4-4789-9cb8-71a577f149c6.jpg" />&#160;and slip angle<img src="4-4900186\3a92f823-8417-4d5e-bc1f-83976d98b998.jpg" />. The rate of longitudinal slip and slip angle of the tire can be calculated by the formula:</p><disp-formula id="scirp.30867-formula96513"><label>(55)</label><graphic position="anchor" xlink:href="4-4900186\f632c810-62c2-43c3-9bb7-1d4bbb8db6f7.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\3eb8c863-6417-469a-b355-f2b358e63955.jpg" /></p><disp-formula id="scirp.30867-formula96514"><label>(56)</label><graphic position="anchor" xlink:href="4-4900186\5117be65-a682-4b9c-b0de-70070fab1ded.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\e2011264-84d3-4c2a-9fb0-4568dbe2a9bb.jpg" /></p><p>where <img src="4-4900186\dfe10080-0894-4f0c-a271-f5658c0f52ca.jpg" /> is the radius of the wheel and <img src="4-4900186\d8306c11-c720-4c4d-bf30-76562f31c818.jpg" /> the velocity of rotation of the wheel. V<sub>axe</sub> is the velocity of lateral translation of the axis and U<sub>p</sub> is the longitudinal velocity of the tire as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>2.</p><p>The expressions can be evaluated from the velocity of center of mass of the vehicle.</p><disp-formula id="scirp.30867-formula96515"><label>(57)</label><graphic position="anchor" xlink:href="4-4900186\27cb1fef-d080-46ea-8efd-c562ff65658a.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\b7481a2c-d318-42ce-9505-c71921ba943a.jpg" /></p><disp-formula id="scirp.30867-formula96516"><label>(58a)</label><graphic position="anchor" xlink:href="4-4900186\5fbc246a-557e-449b-aebb-6b45874ff7da.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.30867-formula96517"><label>(58b)</label><graphic position="anchor" xlink:href="4-4900186\19b54aea-dfc6-4d59-846a-2933eea3ecca.jpg"  xlink:type="simple"/></disp-formula><sec id="s3_4_1"><title>3.4.1. Tire Vertical Load</title><p>In this study, the vertical load of the tire was modeled as a linear spring. Therefore, the vertical force depended on the spring constant.</p><disp-formula id="scirp.30867-formula96518"><label>(59)</label><graphic position="anchor" xlink:href="4-4900186\04fc6281-d1c6-4eb3-bc8a-db3d65df197b.jpg"  xlink:type="simple"/></disp-formula><p>The tire deflections were calculated from the geometry of the vehicle as follows:</p><disp-formula id="scirp.30867-formula96519"><label>(60)</label><graphic position="anchor" xlink:href="4-4900186\b49236d4-79fd-4a77-80dd-330f1aef0d41.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\1c9ff994-4101-4648-a7d4-d48a5daa2c4f.jpg" /></p><disp-formula id="scirp.30867-formula96520"><label>(61)</label><graphic position="anchor" xlink:href="4-4900186\88ef0060-f5b1-4a1a-8c3a-1a4ff19fb82c.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\71010b4e-facf-4346-9cf5-8d5a4995d8bc.jpg" /></p><p>To calculate the combined forces, a dimensional vector of slip amplitude <img src="4-4900186\f2108e61-e696-4d09-a380-dbd45748fbfc.jpg" /> and direction <img src="4-4900186\8ec83f06-06df-4681-8d8e-d2b18a4a9466.jpg" /> was defined [<xref ref-type="bibr" rid="scirp.30867-ref20">20</xref>] as:</p><disp-formula id="scirp.30867-formula96521"><label>(62)</label><graphic position="anchor" xlink:href="4-4900186\74b80ad7-e329-4bdd-80dc-a8f9d0732744.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\ea0edfbf-e924-4cd6-8cfc-0c3694f1af32.jpg" /></p><p>The coefficients of friction between the tire and the ground, in the case of the combined forces, took the forms below:</p><p><img src="4-4900186\a8588493-e4c3-453a-9dc1-da7164ddaaf3.jpg" /></p><disp-formula id="scirp.30867-formula96522"><label>(63)</label><graphic position="anchor" xlink:href="4-4900186\fcf18d98-da65-474c-958d-312a88b2514a.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\a6aa6c83-2e0a-4daa-9b87-4e21117c6fa8.jpg" /></p><p>Finally, longitudinal and lateral forces in the case of combined motion were calculated:</p><disp-formula id="scirp.30867-formula96523"><label>(64)</label><graphic position="anchor" xlink:href="4-4900186\be49379f-187a-400b-b829-bfaf0396277c.jpg"  xlink:type="simple"/></disp-formula><p><img src="4-4900186\ee3c2bdc-b713-421e-809c-ce7a68c57702.jpg" /></p></sec><sec id="s3_4_2"><title>3.4.2. Braking Force</title><p>The braking force was calculated by taking into account forces and moments developed in the wheel due to rotation (spin) of the wheel as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>3. Acceleration of rotation (spin) of the wheels <img src="4-4900186\100e72c8-deb1-43fa-9103-e7ac62bb2426.jpg" /> were calculated from the rotational motion of the wheels as follows [<xref ref-type="bibr" rid="scirp.30867-ref21">21</xref>]:</p><disp-formula id="scirp.30867-formula96524"><label>(65)</label><graphic position="anchor" xlink:href="4-4900186\c7cc2387-572b-40ee-8679-82f98da1308a.jpg"  xlink:type="simple"/></disp-formula></sec></sec></sec><sec id="s4"><title>4. Vehicle Model Validation</title><p>The TruckSim software, developed by the transportation center of the University of Michigan (UMTRI), is specialized in the simulation of heavy vehicles [15,19,22]. The center also developed software applications: CarSim for tourist vehicles and BikeSim for motorcycles. TruckSim, the most popular software in this field, was used to represent and study the dynamics of vehicles in a computer environment. It is possible to analyze a large number of vehicle configurations, since the software has a library of existing models in the transportation industry. However, TruckSim can only add a load that is considered to be fixed on the semi-trailer. This feature does not allow to study the dynamic behavior of liquid sloshing in tanker trucks. The TruckSim library also has a number of predefined trajectories and maneuvers that can enable researchers to validate the behavior of the vehicle model developed, for difficult maneuvers such as motion in a curve, change of single and double lanes. In the TruckSim environment, the maneuvers are predefined paths, i.e., the excitation is represented by a displacement vector. However, for the model developed in this study, the excitation was defined by the angle of steering or braking torque as an input parameter. From the output vector, the response of the steering angle was recorded. This response was the input parameter for our model that considered the same configuration for a unit or articulated vehicle as defined by the Tables 1 and 2 in the annexure [<xref ref-type="bibr" rid="scirp.30867-ref22">22</xref>]. Two lane change maneuvers (single and double) with a constant speed <img src="4-4900186\1879f398-1a5a-4f4b-9d61-5c1b4e7638e3.jpg" />were chosen to compare the two models. <xref ref-type="fig" rid="fig1">Figure 1</xref>4 shows the trajectory and the steer angle during the two maneuvers [<xref ref-type="bibr" rid="scirp.30867-ref22">22</xref>].</p><p>Figures 15 and 16 represent the comparison between model simulations for the unit vehicle and the TruckSim software respectively. The vehicle directional responses were evaluated using two difficult motions, such as change of single and double lanes. This comparison was characterized in terms of roll angle, lateral acceleration of the center of mass and trajectory traveled from the center of mass. The simulation showed a good correla</p><p><xref ref-type="table" rid="table1">Table 1</xref>. Geometric parameters of unit vehicle.</p><disp-formula id="scirp.30867-formula96525"><graphic  xlink:href="4-4900186\6c92c783-ddb9-4ff9-9f65-bf0216f6f35e.jpg"  xlink:type="simple"/></disp-formula><p><xref ref-type="table" rid="table2">Table 2</xref>. Geometric parameters of articulated vehicle.</p><p>(a)</p><p><img src="4-4900186\f8070fbe-f262-458b-ad8b-ea4b5268005e.jpg" /></p><p>(b)</p><p><img src="4-4900186\92c8719d-2d18-4861-957e-f343b8f26ce3.jpg" /></p><p>tion between the two models. A small difference was noted for the trajectory of the center of mass. This difference may be due to the steering angle error of the output vector obtained using TruckSim. In addition, excitement used for the TruckSim software was in closed loop (predefined trajectory).</p><p>In case of articulated vehicles, the analysis was more complicated. This difficulty was due to addition of the hinge point where there were additional forces and moments acting between the tractor and trailer. Figures 17 and 18 represent the comparison between the two models for the same difficult issues such as motions during change of single and double lanes. A good overall correlation was observed. However, our model underestimated the response to some extent. This difference in response was observed due to yaw motion. TruckSim software</p><p>was able to handle such situation in a better way. This difference can be explained based on the assumption that the fifth wheel was considered as a rigid body for our model. However, in TruckSim it was modeled by a spring-damper combination, which can represent multibody connections between subsystems in a better way. The increase in the response of yaw motion influenced</p><p>the trajectory of the vehicle as illustrated by Figures 17 and 18. This may be due to the error of steering angle recorded from the TruckSim output vector. Still, this difference did not practically affect the very good corre lation between the two models.</p></sec><sec id="s5"><title>5. Conclusions</title><p>A complete nonlinear three-dimensional vehicle model was developed and validated by Trucksim software. Both unit vehicle and articulated vehicle combination systems were considered in this study. The model gave realistic results in simulation of handling maneuvers near and beyond the adhesion limits.</p><p>The load&#173;transfer for mobile charge due to the liquid was accurately modeled and integrated into the vehicle model as a multibody system. The dynamic responses of tank vehicles were further investigated in view of variations in vehicle maneuvers, fill volume, road condition, and tank configuration [<xref ref-type="bibr" rid="scirp.30867-ref8">8</xref>].</p><p>This research, can help better understanding of this kind of complex problem. This will make it possible to answer some queries in the field of safety and the stability of the heavy vehicles, in particular for the tanktruck.</p></sec><sec id="s6"><title>REFERENCES</title></sec><sec id="s7"><title>Definitions of Symbols</title><p><img src="4-4900186\415aa9eb-8af7-426e-b1c9-b4de63193f46.jpg" />: Longitudinal velocity of sprung mass<img src="4-4900186\70492369-55ef-4b5a-95d9-7cde8f319a3f.jpg" />;</p><p><img src="4-4900186\7de2643c-cf81-4f0c-a406-fefa8235961e.jpg" />: Lateral velocity of the sprung mass<img src="4-4900186\92a2f3e2-b862-452c-a624-90c9b24b9bbb.jpg" />;</p><p><img src="4-4900186\0899cb2d-06ef-4c68-aef0-5f166cdbe88a.jpg" />: Yaw rate of the sprung mass<img src="4-4900186\5adc4b19-f4ae-476c-ab9c-72a8d2d7e68b.jpg" />;</p><p><img src="4-4900186\8d7e616b-e9f5-4143-bf49-b6dfb5d09be5.jpg" />: Roll rate of the sprung mass<img src="4-4900186\93db8f84-349f-445a-bc60-b41789bfd673.jpg" />;</p><p><img src="4-4900186\6491e6b9-e6cf-4ded-a0c9-2fdcba95b4c6.jpg" />: Distance between the two tires;</p><p><img src="4-4900186\af1bd025-8cde-4f8f-80ce-ee3043061dfb.jpg" />: Distance between the center of mass of the axle <img src="4-4900186\05764f20-2fe2-47d8-bdb5-3790a52b49d6.jpg" /> and the center of (one tire or dual tires);</p><p><img src="4-4900186\2455ab37-9c30-4e1c-ae5f-0213b8f765bb.jpg" />: Longitudinal distance between the center of mass of the axle <img src="4-4900186\1c26b33b-8595-471f-b8ad-48697735997b.jpg" /> and the center of the sprung mass<img src="4-4900186\c92081ad-e6ed-4055-8363-f518be2a6641.jpg" />;</p><p><img src="4-4900186\e36dd767-a28f-4bf8-9138-f2600ba89f2c.jpg" />: Vertical distance between the roll center of the axle <img src="4-4900186\9835e32a-dc4c-464c-939f-7457b0b87991.jpg" /> and the center of the sprung mass<img src="4-4900186\0b024950-fef4-4f21-bcb3-89cfa1bd03b8.jpg" />;</p><p><img src="4-4900186\21215134-1bfb-4c33-98bc-b3468c29c078.jpg" />: Vertical distance between the roll center roll of the axle <img src="4-4900186\fd4ab7d1-f92b-4bb0-88aa-131f6ce94e76.jpg" /> and the road;</p><p><img src="4-4900186\0e3b505c-69bb-4c38-b83f-f3126d9e4ddb.jpg" />: Initial deflection due to static deflection;</p><p><img src="4-4900186\78edd8f8-f1c7-4c26-95e8-30cb3eacaa12.jpg" />: Sprung mass vertical displacement<img src="4-4900186\32fbc1e3-d48a-4a30-bbdd-2784c0ef7a38.jpg" />;</p><p><img src="4-4900186\f03973f6-08dd-4380-8757-b4efaf1cd929.jpg" />: The vertical distance between the roll center and center of the axle<img src="4-4900186\e3581a55-c68b-422b-b42f-4b6eecc6809b.jpg" />;</p><p><img src="4-4900186\98bcb697-a838-4793-b750-2c98432fe603.jpg" />: Initial vertical distance between roll center and center of the axle<img src="4-4900186\5d55ec43-f907-4719-873c-d9677f4ee1a7.jpg" />;</p><p><img src="4-4900186\6d44a7f6-7c51-4da8-a9cf-820747c416a4.jpg" />: The vertical distance between the roll center and center of mass of the sprung mass<img src="4-4900186\e51fbc24-6fda-4d72-b3ff-540dfa2f745a.jpg" />;</p><p><img src="4-4900186\6a3806be-0372-4f42-9060-bd74f08b0689.jpg" />: Moment due to constraints of the fifth wheel;</p><p><img src="4-4900186\fdf8cdf3-8fd2-469e-8b79-c8e186777b01.jpg" />: Moment due to the suspension forces;</p><p><img src="4-4900186\ec10f343-36de-4740-a6cd-1f47fd6eefc3.jpg" />: Wheel drive troque;</p><p><img src="4-4900186\46248da2-2b19-4125-b074-1264be77447c.jpg" />: Engine torque;</p><p><img src="4-4900186\51e9da83-24dc-4758-a447-c5b661972121.jpg" />: Wheel braking torque;</p><p><img src="4-4900186\bb3679ea-0987-4b7f-ba6e-8e3f49017b2e.jpg" />: Wheel moment of inertia;</p><p><img src="4-4900186\16a2c1de-06d2-4e78-9f6b-abd4edbfc22d.jpg" />: Transmission ratio;</p><p><img src="4-4900186\cbfc3c5f-f635-492d-a9a5-c8065997677b.jpg" />: Diff&#233;rentiel ratio;</p><p><img src="4-4900186\7192a419-3094-46be-aac2-1871cbb07891.jpg" />: Torque function (the fraction of engine torque applied to the specific wheel);</p><p><img src="4-4900186\a362d11c-9656-4810-b464-78e46adefdd0.jpg" />: Longitudinal tire-road contact force;</p><p><img src="4-4900186\559087f3-999c-47cf-8ba0-f69a91968710.jpg" />: Resistance moment of the tire.</p></sec><sec id="s8"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.30867-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">J. 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