A missile control system can avoid instability at high angles of attack by cross-coupling roll and steering sensor signals between the steering and roll channels. The control law for the system is derived by use of the Model-in-the-Performance Index Technique which makes the system respond at high angles as it does at low angles with desired response times, bandwidths, and stability.
High Angle-of-Attack Missile Control System for Aerodynamically Controlled Missiles
1978
14 pages
Report
No indication
English
Missile Guidance & Control Systems , Ordnance , Patents , Guided missiles , Flight control systems , Pitch(Motion) , Roll , Yaw , Aerodynamic forces , Coupling(Interaction) , Feedback , Kinematics , Steering , Aerodynamic stability , Angle of attack , PAT-CL-244-3.21 , High angle of attack , Cross coupling
Minimum Energy Guidance for Aerodynamically Controlled Missiles
Tema Archive | 2011
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