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
2008-07-01
4366066 byte
Conference paper
Electronic Resource
English