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This article is cited in 2 scientific papers (total in 2 papers)
Trim angle of attack determination and altitude correction in the TAUS-MC algorithm
A. S. Samotokhin
Abstract:
Algorithms for determination of actual trim angle of attack and altitude correction of inertial navigation errors are suggested. Both algorithms are a part of onboard TAUS-MC algorithm of vehicle motion control at reentry trajectories from the Moon with range of 10000 km and two atmospheric phases.
Keywords:
terminal control, reentry at return from the Moon, skip-up trajectory,
trim angle of attack, errors of inertial navigation.
Citation:
A. S. Samotokhin, “Trim angle of attack determination and altitude correction in the TAUS-MC algorithm”, Keldysh Institute preprints, 2020, 108, 20 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2899 https://www.mathnet.ru/eng/ipmp/y2020/p108
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