Equations given connection between criteria coefficients, control law, coordinates vectors of errors and the work of an inertial actuating link during transient process of a constant disturbing acceleration compensation for the case of a plain rotation movement are obtained. Unlike traditional form of a control law that in article takes in account all coordinates of the state vector according to chosen model what has a positive influence on stability factor and stabilization accuracy. Obtained results give the possibility to determine control law coefficients on the assumption of taken priority system’s indexes.
PERFORMANCE CRITERION OF A TRANSIENT PROCESS AND ACCURACY FIGURES OF A ROCKET STABILIZATION SYSTEM
2017
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
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Development of stabilization system for viking rocket
Engineering Index Backfile | 1955
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