DMOC approach to solve Goddard rocket problem in comparison with RPM

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

A new approach - DMOC (Discrete Mechanics and Optimal Control) is presented to solve the classic Goddard rocket problem, in comparison with RPM (Radau Pseudospectral Method). DMOC approach firstly discretizes the Lagrange-d'Alembert principle for the rocket system, the resulting forced discrete Euler-Lagrange equations then serve as constraints for the optimization of a given cost functional. Therefore the optimal control problem is converted into a nonlinear programming (NLP) problem. While RPM transcribes the optimal control problem to a NLP problem by parameterizing the state and control using global polynomials and collocating the differential-algebraic equations using nodes obtained from a Gaussian quadrature. Finally, DMOC approach and RPM both successfully solve the Goddard rocket problem, which is a terminal free, singular optimal control problem with path constrain; the results proved that DMOC approach and RPM each have its strong points.

源语言英语
主期刊名Proceedings of the 32nd Chinese Control Conference, CCC 2013
出版商IEEE Computer Society
2185-2189
页数5
ISBN(印刷版)9789881563835
出版状态已出版 - 18 10月 2013
活动32nd Chinese Control Conference, CCC 2013 - Xi'an, 中国
期限: 26 7月 201328 7月 2013

出版系列

姓名Chinese Control Conference, CCC
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议32nd Chinese Control Conference, CCC 2013
国家/地区中国
Xi'an
时期26/07/1328/07/13

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