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- W3023026103 abstract "Abstract The conception of the Attitude Control System (ACS) is described for the spacecraft (SC) designed for exploration of the planets of the Solar System. Particularities of Mars mission are noted. The multi-functionality of the ACS is a particularity of the ACS for the future mission, i.e. control of the SC injection into the trajectory of flight to Mars, the SC attitude control during transit, control of the probes release for their landing onto the Mars surface, as well as control of the on-board automated equipment, high gain antenna actuator etc. The problems are discussed reflecting the phases of the System development and procedure of the ground testing providing the cycles of the hardware and software tests in all possible extreme modes taking into account the real program of flight to Mars. The procedure of the ACS interaction with the ground control station is discribed. The procedure of development and ground testing of the ACS is as a result of experience accumulated during many years in such the programs as missions to Venus, Mars, Phobos." @default.
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- W3023026103 date "1993-01-01" @default.
- W3023026103 modified "2023-09-27" @default.
- W3023026103 title "ATTITUDE CONTROL SYSTEM OF THE AUTONOMOUS SPACECRAFT “MARS”, DEVELOPMENT, GROUND VALIDATION AND VERIFICATION, FLIGHT CONTROL OPERATION" @default.
- W3023026103 doi "https://doi.org/10.1016/b978-0-08-041715-8.50023-7" @default.
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