Multi-point powered descent guidance based on optimal sensitivity

Author:

Ma LinORCID,Wang Kexin,Xu Zuhua,Shao Zhijiang,Song Zhengyu,Biegler Lorenz T.

Funder

National Natural Science Foundation of China

State Key Laboratory Project of China

Joint Innovation Fund of the China Academy of Launch Vehicle Technology and Universities

Fundamental Research Funds for the Central Universities

Equipment Pre-Research Project of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Lossless convexification of nonconvex control bound and pointing constraints of the soft landing optimal control problem;Açıkmeşe;IEEE Trans. Control Syst. Technol.,2013

2. Implementation and experimental demonstration of onboard powered-descent guidance;Scharf;J. Guid. Control Dyn.,2017

3. Interpolation-enhanced powered descent guidance for onboard nominal, off-nominal, and multi-X scenarios;Scharf,2015

4. Trajectory optimization for planetary multi-point powered landing;Ma,2017

5. Flight testing of terrain-relative navigation and large-divert guidance on a VTVL rocket;Trawny,2015

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