DocumentCode :
2383364
Title :
Embedded autopilot for accurate waypoint navigation and trajectory tracking: Application to miniature rotorcraft UAVs
Author :
Kendoul, Farid ; Zhenyu, Yu ; Nonami, Kenzo
Author_Institution :
Dept. of Electron. & Mech. Eng., Chiba Univ., Chiba, Japan
fYear :
2009
fDate :
12-17 May 2009
Firstpage :
2884
Lastpage :
2890
Abstract :
In this paper, we describe a miniature flight platform weighing less than 700 grams and capable of way-point navigation, trajectory tracking, precise hovering and automatic takeoff and landing. In an effort to make advanced autonomous behaviors available to mini and micro rotorcraft, a lightweight/portable and inexpensive Guidance, Navigation, and Control system (GN&C) was developed. To compensate for the weaknesses of the low-cost equipment, we put our efforts in obtaining a reliable model-based nonlinear controller. The GN&C system was implemented on a small four rotor helicopter which has undergone an extensive program of flight tests, resulting in various flight behaviors under autonomous control from takeoff to landing. Flight test results that demonstrate the operation of the GN&C algorithms on a real MAV are presented.
Keywords :
aerospace control; aircraft navigation; helicopters; nonlinear control systems; position control; remotely operated vehicles; GN&C; accurate waypoint navigation; automatic landing; automatic takeoff; guidance navigation-and-control system; miniature flight platform; miniature rotorcraft UAV; reliable model-based nonlinear controller; trajectory tracking; unmanned aerial vehicle; Aerospace electronics; Automatic control; Control systems; Hardware; Navigation; Payloads; Remotely operated vehicles; Rotors; Trajectory; Unmanned aerial vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Automation, 2009. ICRA '09. IEEE International Conference on
Conference_Location :
Kobe
ISSN :
1050-4729
Print_ISBN :
978-1-4244-2788-8
Electronic_ISBN :
1050-4729
Type :
conf
DOI :
10.1109/ROBOT.2009.5152549
Filename :
5152549
Link To Document :
بازگشت