Integrated Targeting and Guidance for Powered Planetary Descent

Author:

Azimov Dilmurat M.ORCID,Bishop Robert H.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference32 articles.

1. Apollo 12 mission report, trajectory reconstruction and post-flight analysis, vol. 1, NASA-TM-x-70272, houston, TX, 1970

2. Azimov, D.M.: Automated, real-time targeting and guidance software for lunar-descent and precision landing. Final report. ARTGUID 2009-07-22. NASA SBIR phase I. Contract NNX09CE29p, pp. 53 (2009)

3. Paschall, S., Brady, T., Fill, T., Sostaric, R.: Lunar landing trajectory design for onboard hazard detection and avoidance. In: 32nd Annual AAS Guidance and Control Conference, Breckenridge, CO (2009)

4. Christensen, D., Geller, D.: Terrain-relative and beacon-relative navigation for lunar powered descent and landing. J. Astronaut. Sci. 58(1), 121–151 (2011)

5. Blackmore, L., Acikmese, B., Scharf, D.P.: Minimum-landing-error powered-descent guidance for mars landing using convex optimization. Guid. Control Dynam. 33(4), 1161–1171 (2010)

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