AIAA Guidance, Navigation, and Control Conference 2014
DOI: 10.2514/6.2014-0977
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Safety Critical Platform for Mini UAS Insertion into the Common Airspace

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Cited by 11 publications
(7 citation statements)
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“…The next section briefly introduces the vision system and methods applied onboard our UAV in S& A flight test experiences (for details of the UAV see [13]). VI.…”
Section: Sil Simulation Test Campaignmentioning
confidence: 99%
“…The next section briefly introduces the vision system and methods applied onboard our UAV in S& A flight test experiences (for details of the UAV see [13]). VI.…”
Section: Sil Simulation Test Campaignmentioning
confidence: 99%
“…It consists of the conventional components which are necessary for outdoor navigation, such as accelerometer, rate gyro, differential and absolute pressure sensor, magnetometer and a GPS unit [15].…”
Section: B Inertial Measurement Unit Modelmentioning
confidence: 99%
“…The EGT served as a very simple rendering engine, calculating only the camera images and the feature point locations on realistic flight paths generated in our hardware-in-the-loop simulator [15]. Two kind of paths are used: 1) a sinusoidal trajectory and 2) a zig-zag path, both with nearly constant altitude.…”
Section: A Simulation Environmentmentioning
confidence: 99%
“…In our system the conventional accelerometer, rate gyro, differential and absolute pressure sensor and magnetometer are completed with a GPS unit [17].…”
Section: B Imu Modelsmentioning
confidence: 99%