A State-Dependent Riccati Equation Approach to Atmospheric Entry Guidance-Reference-Cited by-同舟云学术

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A State-Dependent Riccati Equation Approach to Atmospheric Entry Guidance

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Steinfeldt Bradley¹,Tsiotras Panagiotis¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8310

Reference19 articles.

1. 2B.Steinfeldt,M.Grant,D.Matz,R.Braun,andG.Barton,“Guidance,Navigation,andControlTechnologySystemTradesforMarsPinpoint Landing,”AIAAPaper2008-6216,August2008.

2. 3G.Carman,D.Ives,andD.Geller,“Apollo-DerivedMarsPrecisionLanderGuidance,”AIAAPaper98-4570,August2002.

3. 4G.MendeckandG.Carman,“GuidanceDesignforMarsSmartLandersUsingtheEntryTerminalPointController,”AIAAPaper2008-6216, August2008.

4. 5R.Chambers,“SevenVehiclesinOne: OrionGN&C,”AIAAPaper2008-7744,September2008.

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