Aeroelastic stability of aircraft equipped with automatic pilot; method is proposed for determining domain in which some adjustable parameters of autopilot may vary without risk of instability; equation of domain boundary in n-dimensional space of parameters is simple matrix equation; boundary deformation under effect of autopilot's gain variations is examined; boundary analysis gives best positions for detectors and indicates type of compensating circuit necessary to stabilize aircraft.
Stabilite aeroelastique d'avions equipes de pilote automatique
Stabilite aeroelastique d'avions equipes de pilote automatique
Revue Francaise de Mecanique ; n 15
1965
7 pages
Article (Journal)
French
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