DocumentCode :
2624083
Title :
On the development of GNC algorithm for a high-glide payload delivery system
Author :
Kaminer, Isaac I. ; Yakimenko, Oleg A.
Author_Institution :
Dept. of Mech. Eng., Naval Postgraduate Sch., Monterey, CA, USA
Volume :
5
fYear :
2003
fDate :
9-12 Dec. 2003
Firstpage :
5438
Abstract :
The paper considers the development and simulation testing of the control algorithms for an autonomous high-glide aerial delivery system, which consists of 650 sq. ft rectangular double-skin parafoil and 500lb payload. The paper starts with the optimal control analysis and applies it further to the real-time trajectory generation. Resulting guidance and control system includes tracking this reference trajectory using a nonlinear tracking controller. The paper presents the description of the algorithm along with simulation results.
Keywords :
control system analysis; control system synthesis; missile guidance; navigation; nonlinear control systems; optimal control; simulation; tracking; autonomous high glide aerial delivery system; double skin parafoil; high glide payload delivery system; missile guidance; navigation; nonlinear tracking controller; optimal control system analysis; real time trajectory generation; simulation; Actuators; Computational modeling; Control systems; Mechanical engineering; Navigation; Nonlinear control systems; Optimal control; Payloads; System testing; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2003. Proceedings. 42nd IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7924-1
Type :
conf
DOI :
10.1109/CDC.2003.1272502
Filename :
1272502
Link To Document :
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