Minimum-Fuel Powered Descent for Mars Pinpoint Landing

Author:

Topcu Ufuk1,Casoliva Jordi1,Mease Kenneth D.1

Affiliation:

1. University of California, Irvine, California 92697-3975

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 52 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Rethinking Propellant-Optimal Powered Descent Guidance;Journal of Guidance, Control, and Dynamics;2024-09-03

2. Fuel-optimal powered descent guidance for lunar pinpoint landing using neural networks;Advances in Space Research;2024-07

3. Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles;Journal of Guidance, Control, and Dynamics;2023-03

4. Optimal planetary landing with pointing and glide-slope constraints;2022 IEEE 61st Conference on Decision and Control (CDC);2022-12-06

5. Theoretical Analysis of Fuel-Optimal Powered Descent Problem with State Constraints;Journal of Guidance, Control, and Dynamics;2022-12

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