FIELD: astronautics.
SUBSTANCE: when controlling the spacecraft using a sound onboard computer when entering the shadow section, starting the timer provided in the spacecraft control unit with a duration equal to the maximum duration of the shadow section; after exiting from the shadow section with the faulty on-board computer, by the timer signal, the spacecraft is switched to the operation mode using the autonomous control loop, and in good on-board computer, according to information from on-board ballistic software, timer is disconnected, and spacecraft control is performed based on information of serviceable on-board computer.
EFFECT: providing orientation of solar panels relative to direction to the Sun after exiting orbital shadow section even in case of failure of on-board computer operation.
1 cl
| Title | Year | Author | Number |
|---|---|---|---|
| SPACECRAFT ORIENTATION METHOD | 2019 |
|
RU2720577C1 |
| METHOD OF ORIENTATION OF SPACECRAFT | 2020 |
|
RU2736522C1 |
| METHOD FOR CONTROLLING THE ORIENTATION OF THE SPACECRAFT | 2021 |
|
RU2760818C1 |
| METHOD FOR ORIENTATION OF ARTIFICIAL EARTH SATELLITE | 2013 |
|
RU2544021C2 |
| METHOD AND DEVICE FOR CONTROLLING MOTION OF A SPACECRAFT WITH CONTROLLED ORIENTATION | 2017 |
|
RU2669481C1 |
| NAVIGATION SATELLITE ORIENTATION METHOD | 2014 |
|
RU2569999C2 |
| METHOD OF CONTROLLING SPACE VEHICLE SUN BATTERY POSITION | 2008 |
|
RU2361788C1 |
| METHOD OF CONTROLLING SPACECRAFT FOR REMOTE EARTH SENSING | 2019 |
|
RU2722598C1 |
| METHOD OF CONTROLLING ORIENTATION OF SOLAR PANELS OF LOW-ORBITING SPACECRAFT BASED ON GENERATED CURRENT | 2014 |
|
RU2578416C1 |
| DIRECT CURRENT POWER SUPPLY METHOD IN AUTONOMOUS POWER SUPPLY SYSTEM OF SPACE DEVICE AND SPACE DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2677963C1 |
