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.
Disturbance Rejection in Approach and Landing Trajectory Generation for RLVs
01.07.2008
4366066 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch