Plant equations, autopilot structure and control philosophy are described for the roll control of a vehicle that has destabilizing roll-yaw coupling. Computer-implemented stability analyses and transient responses for two autopilot designs are presented and discussed. (ERA citation 05:004803)
Roll Control of an Attitude-Controlled Aerodynamic Vehicle Which Has Strong Roll-Yaw Coupling
1979
41 pages
Report
Keine Angabe
Englisch
Roll-attitude control of a missile having a strong aerodynamic non-linearity
Tema Archiv | 1980
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