A mathematical model is developed and analytical evaluations are made for angular revolutions of a (return space vehicle) RSV during formation of the stable balance equilibrium on large angles of attack without applic...
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A mathematical model is developed and analytical evaluations are made for angular revolutions of a (return space vehicle) RSV during formation of the stable balance equilibrium on large angles of attack without application of control moment. The special balance mode permits RSV to widen a touchdown area after orbital departure. Results obtained are of practical significance in designing of promising RSVs including reusable launch vehicles for servicing ISS and in development of program and algorithm software including an onboard control algorithm to orient the lift force in space.
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