For certain structural failures and damages for which redundancy cannot be employed, the best method to ensure flight safety is the self-repairing technique. Based on the characters of self-repair plane, the paper explicitly states some basic assumptions of the self-repair, and comes up with some new concepts: control input, operating input, command input, repair input and operating and control factor, etc., and their relationship. Thus it provides a simple and reliable mathematical model structure for the research on the self-repair control of plane.
Some basic problems about self-repairing flight control
2000-01-01
395596 byte
Conference paper
Electronic Resource
English
Some Basic Problems about Self-Repairing Flight Control
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