MEMS-Based Low-Cost Flight Control System for Small UAVs

Abstract Small unmanned air vehicles (UAVs) can be used for various kinds of surveillance and data collection missions. The UAV flight control system is the key to a successful mission. This paper describes a low-cost micro-electro mechanical system-based flight control system for small UAVs. The integrated hardware flight control system weighs only 24 g. The system includes a highly-integrated wireless transmission link, which is lighter than traditional links. The flight control provides altitude hold control and global positioning system navigation based on gain scheduling proportional-integral-derivative control. Flight tests to survey the grass quality of a large lawn show that the small UAV can fly autonomously according to a series of pre-arranged waypoints with a controlled altitude while the wireless video system transmits images of the surveillance target to a ground control station.

[1]  S. M. Smith,et al.  Performance results of a fuzzy behavioral altitude flight controller and rendezvous and docking of an autonomous underwater vehicles with fuzzy control , 1996, Proceedings of Symposium on Autonomous Underwater Vehicle Technology.

[2]  Karl Johan Åström,et al.  Adaptive Control , 1989, Embedded Digital Control with Microcontrollers.

[3]  R. Fink,et al.  Design and Development of a Low-Cost Test-Bed for Undergraduate Education in UAVs , 2005, Proceedings of the 44th IEEE Conference on Decision and Control.

[4]  Jiang Guo-hua Simulation & Experiment System of Space Manual Control- Rendezvous and Docking Based on Virtual Reality , 2002 .

[5]  Zhaoying Zhou,et al.  Micro air vehicle: configuration, analysis, fabrication, and test , 2004 .

[6]  Michael Matessa,et al.  Fault management during dynamic spacecraft flight: effects of cockpit display format and workload , 2005, 2005 IEEE International Conference on Systems, Man and Cybernetics.

[7]  Lian Shun-guo Study on Performance of Integration Control by Man and Machine in Stage of Final Approaching for Spaceship Rendezvous and Docking , 2006 .

[8]  Dong Sun,et al.  Model identification of a micro air vehicle in loitering flight based on attitude performance evaluation , 2004, IEEE Transactions on Robotics.

[9]  John B. Davidson,et al.  SIMULATION AND FLIGHT CONTROL OF AN AEROELASTIC FIXED WING MICRO AERIAL VEHICLE , 2002 .

[10]  Qi Nai INVESTIGATION OF SIMULATION TESTING PROJECT ON RENDEZVOUS AND DOCKING , 2000 .

[11]  S. Seereeram,et al.  Vision-based relative pose estimation for autonomous rendezvous and docking , 2006, 2006 IEEE Aerospace Conference.

[12]  Wu Hong Several questions on autonomous rendezvous docking , 2003 .

[13]  Derek Kingston Implementation Issues of Real-Time Trajectory Generation on Small UAVs , 2004 .

[14]  Timothy W. McLain,et al.  Autonomous Vehicle Technologies for Small Fixed-Wing UAVs , 2003, J. Aerosp. Comput. Inf. Commun..

[15]  Hongbing Zhu,et al.  An Autonomous Flight Control Strategy Study of a Small-Sized Unmanned Aerial Vehicle , 2005, IEICE Trans. Electron..