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Chen, Q. (2009) Numerical Simulation of Aircraft Pitch Motion and Rudder Surface Control. China Aerodynamics Research and Development Center. https://kns.cnki.net/kcms2

has been cited by the following article:

• TITLE: Aerodynamic, Kinematic and Control Coupling Simulation of Aircraft Maneuvering Flight

  AUTHORS: Haohui Tang, Shuanghou Deng

  KEYWORDS: High Angle of Attack Pull-Up, High Maneuvering Aircraft, Flight Attitude Control Rate, Dynamic Unstructured Nested Mesh, Virtual Flight Simula-tion Platform

  JOURNAL NAME: World Journal of Engineering and Technology, Vol.12 No.4, November 27, 2024

  ABSTRACT: Aiming at the high angle of attack pull-up and multi-channel roll pull-up coupling problems of high maneuvering aircraft, this paper establishes the flight attitude control rate by means of unsteady flow numerical solution, dynamic unstructured nested mesh assembly method and numerical solution method of flight mechanics equation. On this basis, a virtual flight simulation platform integrating pneumatics, motion and control is established. Based on this virtual flight simulation platform, F-16 aircraft is simulated by high angle of attack pull-up flight mode and multi-channel roll pull-up coupling flight mode. Finally, the influence of rudder on the yaw control channel is investigated. The results show that the numerical virtual flight simulation platform established in this paper has the ability to simulate maneuvering flight of aircraft.