This paper describes the design and development of a feedback system for controlling the dynamics of a flapping wing nano air vehcile (NAV). A model of the vehicle dynamics and models of sensors and unique actuator mechanisms are built. An extended Kalman filter is designed to eliminate the effects of sensor bias on state estimation. Results of this study demonstrate stability and yield responses that are approaching desired performance capabilities.
Onboard Stability Control System for a Flapping Wing Nano Air Vehicle
2009
24 pages
Report
Keine Angabe
Englisch
Nano air vehicles , Flight control systems , Kalman filtering , Naval aircraft , Aircraft , Flapping flight , Wings , Aerodynamic stability , Stabilization systems , Actuators , Bio-inspired flight , Feedback control , Feedback , Nanotechnology , Detectors , Avionics , Performance(Engineering) , Algorithms
Flapping-wing air vehicle driving device and flapping-wing air vehicle
Europäisches Patentamt | 2022
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