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·Ix )ω0 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.
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR SPACE VEHICLE WITH FIXED PANELS OF SOLAR BATTERIES ORIENTATION CONTROL DURING EXPERIMENTS ON ORBITS WITH MAXIMUM ECLIPSE PERIOD | 2010 |
|
RU2457158C2 |
| METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE | 2015 |
|
RU2594057C1 |
| METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE | 2015 |
|
RU2594054C1 |
| METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE | 2015 |
|
RU2594056C1 |
| METHOD FOR UNIAXIAL ORIENTATION OF AN ELONGATED SPACE VEHICLE | 2020 |
|
RU2764815C1 |
| METHOD OF SPACECRAFT ORIENTATION WHEN CONDUCTING EXPERIMENTS WITH SCIENTIFIC EQUIPMENT FOR THE STUDY OF CONVECTION | 2014 |
|
RU2581281C2 |
| METHOD OF CONTROLLING ORIENTATION OF SPACECRAFT WITH FIXED SOLAR PANELS WHEN CONDUCTING EXPERIMENTS | 2014 |
|
RU2562904C1 |
| CONTROL OVER ORIENTATION OF SUPPLY SPACESHIP WITH STATIONARY SOLAR BATTERY PANELS AT JOBS UNDER CONDITIONS OF SPINNING | 2013 |
|
RU2539266C2 |
| METHOD FOR DETERMINING INERTIA TENSOR OF SPACECRAFT IN FLIGHT | 2014 |
|
RU2587764C2 |
| METHOD OF CONTROLLING ORIENTATION OF SPACECRAFT WITH FIXED SOLAR PANELS WHEN CONDUCTING EXPERIMENTS ON ORBITS WITH MAXIMUM DURATION OF ECLIPSE PERIOD | 2014 |
|
RU2562903C1 |
