DocumentCode :
2429591
Title :
TAEM guidance for a re-entry vehicle using feedback linearization
Author :
Baek, Joha ; Kim, Jonghun ; Cho, Kyeumrae ; Lee, Dae Woo
Author_Institution :
Pusan Nat. Univ., Busan
fYear :
2007
fDate :
17-20 Oct. 2007
Firstpage :
1420
Lastpage :
1425
Abstract :
This paper investigates an optimal trajectory and a feedback linearization control for a reentry vehicle during TAEM (terminal area energy management) phase. Firstly, an optimization algorithm with dynamic pressure as a cost function is used to obtain optimal trajectory in TAEM. This optimal trajectory is considered as the reference one to ensure stable flight path of the reentry vehicle. The control inputs are the angle of attack and bank angle that determine the total energy and safety of the reentry vehicle. Secondly, feedback linearization is used to design a tracking law in TAEM phase. This paper presents a validity of optimal solution as a reference trajectory with HAC (heading alignment cylinder) and tracking performance of the reentry vehicle onto the reference trajectory by feedback linearization.
Keywords :
feedback; optimal control; position control; space vehicles; dynamic pressure; feedback linearization control; heading alignment cylinder; optimal trajectory; optimization algorithm; reentry vehicle; terminal area energy management; Aerospace engineering; Control systems; Energy management; Engine cylinders; Linear feedback control systems; Navigation; Optimal control; Space vehicles; Trajectory; Vehicle safety; Feedback linearization; Optimization; Re-entry Vehicle; TAEM Phase;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems, 2007. ICCAS '07. International Conference on
Conference_Location :
Seoul
Print_ISBN :
978-89-950038-6-2
Electronic_ISBN :
978-89-950038-6-2
Type :
conf
DOI :
10.1109/ICCAS.2007.4406561
Filename :
4406561
Link To Document :
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