Use of relative-motion invariants to monitor the performance of the measuring instruments of a docking system

Mathematics – Probability

Scientific paper

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Equations Of Motion, Instrument Errors, Spacecraft Control, Spacecraft Docking, Spacecraft Instruments, Spacecraft Reliability, Angular Velocity, Coordinates, Gravitational Fields, Invariant Imbeddings, Probability Theory

Scientific paper

Modern spacecraft control systems require the development of reliability indices that differ qualitatively from the requirement of reliability in the traditional sense. For systems which measure the parameters of relative motion, examined in the present paper, an important index may be one that eliminates the risk involved in the use of unreliable information by detecting possible system malfunctions. The approach proposed to this problem in the case of docking is to use a-priori information on the interrelationship of the various measurable parameters, in particular, the information contained in the equations of relative motion.

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