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Powered Flight Design and Performance Summary for the Mars Science Laboratory Mission

  • Published:2014-07 Issue:4 Volume:51 Page:1197-1207
  • ISSN:0022-4650
  • Container-title:Journal of Spacecraft and Rockets
  • language:en
  • Short-container-title:Journal of Spacecraft and Rockets

Author:

Sell Steven W.1,Davis Jody L.2,Miguel San Martin A.3,Serricchio Frederick3

Affiliation:

1. Mars Science Laboratory, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

2. Atmospheric Flight and Entry Systems Branch, NASA Langley Research Center, Hampton, Virginia 23681

3. Guidance, Navigation, and Control Chief Engineer, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 5 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. A Fast Algorithm for Onboard Atmospheric Powered Descent Guidance;IEEE Transactions on Aerospace and Electronic Systems;2023

2. Powered-descent landing GNC system design and flight results for Tianwen-1 mission;Astrodynamics;2022-01-04

3. Minimum-Fuel Closed-Loop Powered Descent Guidance with Stochastically Derived Throttle Margins;Journal of Guidance, Control, and Dynamics;2021-03

4. Uncertainty Quantication and Control During Mars Powered Descent and Landing using Covariance Steering;2018 AIAA Guidance, Navigation, and Control Conference;2018-01-07

5. Getting to Mars;The Design and Engineering of Curiosity;2018
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