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
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