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
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;
Conference_Titel :
Aerospace and Electronics Conference, 2008. NAECON 2008. IEEE National
Conference_Location :
Dayton, OH
Print_ISBN :
978-1-4244-2615-7
Electronic_ISBN :
7964-0977
DOI :
10.1109/NAECON.2008.4806534
