会议专题

Abort Trajectory Optimization Using an hp-Adaptive Pseudospectral Method

Mission abort scenarios of RLV due to an engine failure which leads to engine cut-off are considered. The abort trajectory optimization problem is treated as a maximum range problem for abort capability analysis. An hp-adaptive pseudospectral method be employed to solve this problem because of its accuracy and computational efficiency. Fuel jettisoning rate is treated as a optimization parameter. Numerical results show the optimal fuel jettison rate is its maximum value and the maximum longitudinal range achievable with fuel jettisoning is increased by 7.62% when compared to the case without fuel jettisoning.

abort rajectory optimization fuel jettisoning hp-adaptive pseudospectral method

Wenhu Wang Xinguo Li Chenxi Wang

School of Astronautics Northwestern Polytechnical University Xian, China

国际会议

2012 Fifth International Symposium on Computational Intelligence and Design 第五届计算智能与设计国际会议 ISCID 2012

杭州

英文

340-343

2012-10-28(万方平台首次上网日期,不代表论文的发表时间)