DocumentCode
3059002
Title
Disturbance Rejection in Approach and Landing Trajectory Generation for RLVs
Author
Jiang, Zhesheng ; Ordonez, Raul
Author_Institution
Dept. of Electr. & Comput. Eng., Univ. of Dayton, Dayton, OH
fYear
2008
fDate
16-18 July 2008
Firstpage
138
Lastpage
141
Abstract
Safety, reliability and operational costs play important roles in reusable launch vehicle (RLV) program. Our previous works proposed a scheme of motion primitives and neighboring optimal control to deal with on-board failure recovery for a RLV. In this paper, disturbance rejection for system parameters and winds is discussed. Robustification is mostly needed.
Keywords
aircraft landing guidance; optimal control; position control; space vehicles; disturbance rejection; landing trajectory generation; onboard failure recovery; optimal control; reusable launch vehicle program; Costs; Electrical safety; Equations; Network-on-a-chip; Optimal control; Robustness; Space shuttles; Space technology; Vehicle dynamics; Vehicle safety;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 2008. NAECON 2008. IEEE National
Conference_Location
Dayton, OH
ISSN
7964-0977
Print_ISBN
978-1-4244-2615-7
Electronic_ISBN
7964-0977
Type
conf
DOI
10.1109/NAECON.2008.4806534
Filename
4806534
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