A six-degree-of-freedom guidance and control analysis of Mars aerocapture-Reference-Cited by-同舟云学术

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A six-degree-of-freedom guidance and control analysis of Mars aerocapture

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

POWELL RICHARD¹,BRAUN ROBERT¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-736

Reference7 articles.

1. 2Bnun,R.D.,andPowell,RW."A Predictor-CorrectorGuidanceAlgorithmforUseinHigh-EnergyAerobrakingSystem Studies,"AIAAPaperNo.91-0058,January 1991.

2. W.L,"MeasuredandPredictedAerodynamicCoefficients and Shock Shapes for Aeroassist night Experiment Configuration,"NASATP-2956,1990.

3. 6h?ahesh, J .IC,Konar. A E.andWardM. D. "Interactive FlightConmlSystem AnalysisProgram,"NASACR-172352, 1984.

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3. Blended control, predictor–corrector guidance algorithm: an enabling technology for Mars aerocapture;Acta Astronautica;2004-03

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