An image of a fabricated eMote is shown in Figure 2. The unique shape of the printed circuit board serves two purposes: to induce auto-rotation and to aspirate the temperature sensor. This shape closely mimics that of the maple seed, or samara, whose evolution naturally selected an asymmetrical seed shape with a long, thin rotor structure and low, off-center center of mass to minimize fall speed and allow airborne seeds to travel farther [19] [20]. In an effort to follow these principles, the center of mass for the eMote is located far below the flexible rotor/antenna structure in order to induce auto-rotation which slows its descent [21]. The final dimensions of both the flexible rotor/antenna structure and

printed circuit board were chosen after iterative testing and refinement of eMote mockups constructed of FR4 and weighted with washers to match the weight distribution. These eMote mock-ups were dropped from various heights in both indoor and outdoor scenarios to determine the size and shape that maximized rotation and minimized fall speed. Additionally, the temperature sensor resides on the small protrusion with ventilation cutouts in order to aspirate the sensor while the eMote is spinning, increasing the accuracy of temperature measurements by isolating the sensor and minimizing thermal bias induced by other components.

The eMote antenna structure serves a secondary purpose as a rotor to enable auto-rotation and slow descent. The structure contains two separate antennas: a 915 MHz Region 2 industrial, scientific, and medical (ISM) band antenna for eMote data transmission and a GPS L1 band antenna, each designed with a larger than necessary bandwidth to allow for manufacturing tolerances. The antennas were designed and fabricated onto a flexible 4 mil Pyralux AP substrate to allow the rotors to bend and flex while falling. The final dimensions of the antenna structure can be seen in Figure 3, where the necessary asymmetry for auto-rotation is clearly visible.

Components for the eMote were chosen in an effort to minimize cost, weight, and power consumption. The main components chosen were the Texas Instruments CC430F5137 embedded microcontroller and ISM band transceiver, Measurement Specialties MS5803 air pressure and temperature sensor, Sensirion SHT25 humidity and temperature sensor, and the u-Blox Max M8 GPS receiver. The GPS module communicates with the microcontroller through a low data rate UART connection to provide a 1 Hz time-stamp alongside GPS coordinates, while the two atmospheric sensors communicate measurements through I²C. These protocols were chosen in an effort to minimize power consumption through the use of the CC430F5137’s low-power modes as discussed in the following subsection. Further, these specific sensors were chosen due to their low cost and acceptable accuracy specifications for data reporting with the World Meteorological Organization (WMO) [22] and National Oceanic and Atmospheric Administration (NOAA) [23]. We estimate that large-scale production of eMotes

could be achieved at a unit cost of around 100 $, much less than other in-situ atmospheric sensing solutions [6] [16] [17].

The eMotes utilize several techniques to reduce power consumption and provide as much data as possible. Onboard the eMotes themselves, UART and I²C are used to minimize power consumption by the microcontroller. The UART interface provides time-stamp and location information from the GPS module once every second that is synchronized by the GPS satellites; this single UART communication wakes the microcontroller from an ultra low-power mode and establishes a synchronized time-stamp across all deployed eMotes. In order to collect data each second, a single I²C bus is used to communicate with both sensor modules using minimal time in an active mode. The minimization of active peripherals on the eMote reduces power consumption and allows the device to be in ultra low-power modes for more than 50% of the time when reporting data once per second.

In order to receive coherent data from over 2000 eMotes at once, a Multiple Frequency Time-Division Multiple Access (MF-TDMA) scheme is used. As the on-board GPS module provides a synchronized time-stamp every second, all deployed eMotes are able to accurately select a time slot using a simple timer module. Each eMote is given a unique identification signature when it is programmed and uses this signature to determine a time slot and frequency channel for its transmissions. In practice, the eMotes are able to make use of 130 individual channels containing 16 time slots per second within the 915 MHz ISM band. It is worth noting that each additional second added between transmissions adds 20 time slots per channel, as 4 time slots of the first second have been allocated for GPS reception. These additional time slots will allow for the deployment of 2600 additional eMotes for each second added. Furthermore, over-sized time slots and forward error correction codes were used to reduce interference and maximize the effective range of the eMotes [24].

The eMote’s atmospheric sensing capabilities were verified through several test deployments. Figure 4 shows a sample set of data collected from an overnight deployment of 5 eMotes across Auburn University’s campus alongside a Davis Instruments Vantage Pro2 weather station to serve as a reference. eMotes have also been tested in several different climes and deployment scenarios: the aforementioned

overnight test deployments; low altitude, small scale deployments from a drone over rural areas near Auburn, AL; and several kilometer high deployments over New Mexico and Alaska testing facilities in conjunction with Sandia National Labs. Data from these tests have been compared to reference data from other atmospheric sensing systems and organizations, such as the Meteorological Terminal Aviation Routine Weather Report (METAR), to calculate the accuracy of reported eMote data. The calculated accuracies for eMote data and accuracy requirements for data reporting with the WMO [22] and NOAA [23] are shown in Table 2.

Verification of the antenna-rotor structure was carried out in two phases: physical testing of eMote auto-rotation and characterization of the two antennas under different bend conditions.

To test the auto-rotation of the eMote, antenna-rotor structures were attached to eMote mock-ups made from FR4 and weighted with washers to emulate the mass distribution of a fully fabricated eMote. These drop units were then dropped from various altitudes: a 15 m drop from the roof of a campus building, a 16 m indoor drop from the rafters of the campus basketball arena, and 50 m and 100 m drops from a drone over nearby farmland. These drop tests were later repeated with fully fabricated eMotes. The average fall time of both the drop units and fabricated eMotes was found to be 2.51 m/s, which is significantly slower than other in-situ atmospheric measurement systems and allows for more data collection [6] [16] [17].

Characterization of the ISM and GPS L1 band antennas was performed in an anechoic chamber with a Keysight FieldFox N9951A and Diamond Antenna Measurement Systems DAMS7000. Figure 5 shows the measured and simulated antenna patterns; the antenna-rotor structure has been designed so that the nulls point to the horizon during free-fall, maximizing GPS satellite signal reception from satellites above and eMote data transmission towards a ground station below. Further, the voltage standing wave ratio (VSWR) was measured for different bend angles of the antenna-rotor structure, as shown in Figure 6, to verify

the designed antennas will still function with a VSWR of less than 2 for the entire ISM and GPS L1 bands for all reasonable bend angles that may occur during free fall.

Long-range eMote operation was verified both in the lab and through actual deployments. In-line attenuators were used inside an anechoic chamber to simulate distance between the eMote and receiver station, yielding a maximum range of roughly 50 km. In order to verify this number in the field, eMotes were attached to balloons and allowed to drift off on the wind. This test was performed several times in different weather conditions to verify long-range operation. The average maximum distance at which valid packets were received for these tests was 14.5 km, with a maximum distance of 18.5 km as shown in Figure 7. This tested range is on the same order of magnitude as that found in laboratory conditions and could potentially be increased by using a different modulation technique or by adding amplifiers to the receiver base station.

The scalability of the MF-TDMA strategy adopted for eMotes was tested through several ground-based large-scale deployments of 44, 80, and 83 eMotes. In each test, the eMotes were run for over 30 minutes to provide a large sample size for assessing the viability of the network. In these tests, packets were received from at least 90% of the deployed eMotes over the course of the test, but only an average of around 60% of sent packets were received. These low packet reception rates are likely due to multipath and interference issues arising from the placement of the eMotes, as both the eMotes and receivers were placed on or near the

ground. Figure 8 shows the placement of eMotes in an intramural field on Auburn University’s campus during the 83 eMote test.