| 摘要 |
PURPOSE: To provide an attitude and orbit control system(AOCS) in which the multiplicity of weight, power consumption, and parts can be reduced, and reliability and flexibility can be increased. CONSTITUTION: One standard interface is respectively arranged between an attitude and orbit control electronic circuit(AOCE) and a peripheral equipment, and between the AOCE and a telecommand/telemetry device. The AOCE and each peripheral equipment are provided with a microprocessor (μP/exp) which can extend a calculating capability. The AOCE is provided with an extendible communication band by inter-point connection. The potential separation of a communication conductor and communication between the twoμP/exp are operated by continuos inter-point connecting parts.
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