|19 Jun 2009
||MATLAB Central Team
By Arthur E. Bryson, Jr., ISBN 0-691-08782-2
This text provides an overview and summary of flight control, focusingon the best possible control of spacecraft and aircraft, i.e., the limitsof control. The minimum output error responses of controlled vehiclesto specified initial conditions, output commands, and disturbances aredetermined with specified limits on control authority. These are determinedusing the linear-quadratic regulator (LQR) method of feedback controlsynthesis with full-state feedback. An emphasis on modeling is also includedfor the design of control systems.