Simulation of the Dynamics of Non- Resonant Motion in a Controlled Descent of an Asymmetric Spacecraft in the Low-density Atmosphere
نویسنده
چکیده
We consider the problem of implementation of non-resonant motion at descent of a spacecraft with small mass and aerodynamic asymmetries in the low-density atmosphere of Mars. A controllable decrease in the mass asymmetry contributes to implementation of non-resonant motion of the spacecraft. We introduce an analytical control law for the magnitude of asymmetry. The results of numerical simulation of spherical motion of a spacecraft with controllable asymmetry are included.
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