METHOD OF UNIAXIAL ORIENTATION OF ELONGATED SPACE VEHICLE Russian patent published in 2012 - IPC B64G1/34 

Abstract RU 2457159 C2

FIELD: transport.

SUBSTANCE: invention relates to space vehicle (SV) orientation control and can be used during experiments and investigations on its board. The method includes gravitational SA orientation after which SV spin around SV axis registered with the Earth centre is performed. Spin is performed with angular velocity of ωx = (Iyz / 5·Ix0 until required time moment, where Iyz is average value of close in value SV inertia moments around OY and OZ transversal axes; Ix is SV inertia moment around longitudinal axis; ω0 is absolute angular velocity of orbital coordinate system.

EFFECT: higher accuracy of uniaxial SV orientation and lowering g level acting on SV during its flight.

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RU 2 457 159 C2

Authors

Babkin Evgenij Vjacheslavovich

Beljaev Mikhail Jur'Evich

Brjukhanov Nikolaj Al'Bertovich

Sazonov Viktor Vasil'Evich

Matveeva Tat'Jana Vladimirovna

Tsvetkov Vjacheslav Vladimirovich

Dates

2012-07-27Published

2010-08-30Filed