The paper is concerned with the initial evaluation of a self adaptive autostabilization system for an airborne vehicle whose dynamic behaviour may vary rapidly and over a wide range during normal operation. The basic design approach could be applied to any airborne vehicle which warranted adaptive control operation, but it is evaluated here in relation to the control of a high performance missile during an 80 second mission. This mission includes a rocket boost phase with accompanying large variations in the model parameters caused by changes in dynamic pressure, mach number, altitude and mass. The adaptive system can be considered as a second generation adaptive scheme in the sense that it provides a logical self-adaptive successor to the well known 'schedule adaptive' systems used heretofore.
A second generation adaptive autostabilization system for airborne vehicles
Ein adaptives Autostabilisierungssystem der zweiten Generation fuer Raumfahrzeuge
Automatica, Oxford ; 17 , 3 ; 459-470
1981
12 Seiten, 9 Bilder, 1 Tabelle, 33 Quellen
Article (Journal)
English
Landing cushioning analysis of new generation heavy airborne armored vehicles
Emerald Group Publishing | 2024
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