General methods for the initial stages of designing control systems of aircraft, missile, and spacecraft complexes are presented. The methods are based on statistical estimates of the characteristics of flight craft and of ground and onboard control system components. Illustrations are taken from foreign technology. Failure rates and standby status of the control systems of aircraft and missile complexes are discussed. Cost effectiveness criteria in the designing of attack and defense aircraft-missile complexes are described and evaluated with examples. Hand-book material presented in the book can be used in the initial stage of designing or in setting up preliminary requirements for systems. The book is written for design engineers and estimator engineers concerned with designing flight craft control systems. (Author)
General Principles of Designing Control Systems
1974
391 pages
Report
No indication
English
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