Optimal Guidance and Control of Lunar Landers with Non-throttable Main Engine

Author:

Oehlschlägel Thimo,Theil Stephan,Krüger Hans,Knauer Matthias,Tietjen Jan,Büskens Christof

Publisher

Springer Berlin Heidelberg

Reference10 articles.

1. Altair lander homepage (2010), http://www.nasa.gov/mission_pages/constellation/news/cece.html

2. Büskens, C., Maurer, H.: SQP-methods for solving optimal control problems with control and state constraints: adjoint variables, sensitivity analysis and real-time control. Journal of Computational and Applied Mathematics 120, 85–108 (2000)

3. Davies, J.L., Striepe, S.A.: Advances in post2 end-to-end descent and landing simulation for the alhat project. AIAA-2008-6938. American Institute of Aeronautics and Astronautics (2008)

4. Fisher, J.L., Striepe, S.A.: Post2 end-to-end descent and landing simulation for the autonomous landing and hazard avoidance technology project - aas 07-119. In: Lunar and Planetary Institute Science Conference Abstracts. Advances in Astronautical Sciences, vol. 127 (2007)

5. Houdou, B.: Next Lunar Lander, Phase A Mission Study, Mission Requirements Document. Tech. Rep. NEXT-LL-MRD-ESA(HME)-0001, ESA (2008)

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