Synthesis of Two-Channel Control to Stabilize the Rotation of a Small Asymmetric Spacecraft in the Martian Atmosphere
Author:
Affiliation:
1. Samara National Research University,Department of Flight Dynamics and Control Systems,Samara,Russia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10168302/10168309/10168482.pdf?arnumber=10168482
Reference38 articles.
1. Asymptotic Analysis of the Stability of the Angle of Attack in an Atmospheric Descent of a Spacecraft with Small Mass and Inertial Asymmetries;lyubimov;12th International Scientific and Technical Conference “Dynamics of Systems Mechanisms and Machines”,2019
2. Optimal Discrete Control Law for Rotation of a Descent Probe with a Small Inertial Asymmetry during the Descent in the Atmosphere of Mars
3. Dynamics and control of angular acceleration of a reentry spacecraft with a small asymmetry in the atmosphere in the presence of the secondary resonance effects;lyubimov;International Siberian conference on control and communications SIBCON Proceedings,2015
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