This article is cited 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.

DOI: 10.20948/prepr-2020-108

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