A three-dimensional predictor–corrector entry guidance based on reduced-order motion equations-Reference-Cited by-同舟云学术

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A three-dimensional predictor–corrector entry guidance based on reduced-order motion equations

Published:2018-02 Issue: Volume:73 Page:223-231
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zeng Liang,Zhang Hongbo,Zheng Wei

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. Apollo Experience Report: Mission Planning for Apollo Entry, Houston, TX;Graves,1972

2. Shuttle entry guidance;Harpold;J. Astronaut. Sci.,1979

3. Adaptive on-board guidance for entry vehicles;Roenneke,2001

4. Entry trajectory design for the X-33 vehicle;Lu,1997

5. Entire flight trajectory design for temporary reconnaissance mission;Lin;Trans. Jpn. Soc. Aeronaut. Space Sci.,2017

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