06-06-2023 дата публикации
Номер: CN116222540A
Принадлежит:
The invention discloses a micro-inertia multi-source autonomous GNC flight control navigation microsystem, method and module. The system comprises a flight control navigation master control center, a power management module, a multi-source sensing measurement module, a safety monitoring module, an execution mechanism module, a communication transceiving module, an online storage module and a metal shell with a mounting hole. The flight control navigation master control center, the power management module, the multi-source sensing measurement module, the safety monitoring module, the execution mechanism module, the communication transceiving module and the online storage module are packaged in a metal shell in a high-density integration mode, and the metal shell is fixedly installed on a micro aerospace vehicle through installation holes. According to the invention, integration and flight control integration of the flight control and navigation functions of the micro aerospace vehicle are ...
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