Disturbance observer-based robust guidance for Mars atmospheric entry with input saturation

Author:

Zheng Yiyu,Cui Hutao

Funder

National Basic Research Program of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference30 articles.

1. Way DW, Davis JL, Shidner JD. Assessment of the Mars Science Laboratory entry, descent, and landing simulation. Proceedings of the 23rd AAS/AIAA space flight mechanics meeting; 2013 Feb 10–14; Kauai HI, USA. Washington, D.C: NASA; 2013. p. 563–81.

2. Entry guidance design and postflight performance for 2011 Mars Science Laboratory mission;Mendeck;J Spacecraft Rockets,2014

3. Mendeck G, McGrew L. Post-flight EDL entry guidance performance of the 2011 Mars Science Laboratory mission. Proceedings of the 23rd AAS/AIAA space flight mechanics meeting; 2013 Feb 10–14; Kauai HI, USA. Washington, D.C.: NASA; 2013. p. 547–62.

4. Brugarolis P, San MAM, Wong E. The entry controller for the Mars Science Laboratory. Proceedings of the 23rd AAS/AIAA space flight mechanics meeting; 2013 Feb 10–14; Kauai HI, USA. Washington, D.C.: NASA; 2013. p. 505–19.

5. Review and prospect of guidance and control for Mars atmospheric entry;Li;Prog Aerosp Sci,2014

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