Aerospace vehicle dynamics and control Book

	Aerospace vehicle modlelling requirements for high bandwidth flight control	1
	Intelligent flight control system	33
	Flight controller design using multivariable loop shaping	81
	Comparison of LQG, H[infinity] and classical designs for the pitch rate control of an unstable military aircraft	103
	A reconfiguration algorithm for real-time aircraft flight control systems	125
	An analytical redundancy scheme for an automatic flight control system	145
	Advanced control of high performance rotorcraft	161
	Design and handling qualities analysis of a full envelope multivariable controller for a combat rotorcraft	181
	Helicopter flight control design: multivariable methods and design issues	199
	An investigation into the phenomenon of helicopter blade sailing	225
	The flight dynamics of an unstable unmanned aircraft	245
	Recent developments in aircraft parameter identification at Delft University of Technology - optimal input design	259
	On the use of a modified step-wise regression method to estimate aircraft stability derivatives from dynamic wind tunnel test data	285
	The performance of CLOS missile systems against weaving targets	311
	The aeroelastic behaviour of a missile control fin with a pneumatic actuation system	331
	Navigation in the vicinity of a comet	349
	Development of a new model with lumped elements for simulation of tethered systems	371
	Proof-mass actuator control of shuttle based astromast	395
	Dynamics of a spinning spacecraft containing liquid propellant	417