Aerospace vehicle dynamics and control: based on the proceedings of a conference organized by the Institute of Mathematics and its Applications on aerospace vehicle dynamics and control, held at the Cranfield Institute of Technology, in September 1992
Clarendon Press, 1994 - Literary Criticism - 438 pages
Rapid developments in computer technology have dramatically affected the analysis, synthesis, and control of aerospace vehicle dynamics. As new challenges emerge in the wake of the recent shift in emphasis from military to civil applications, research concerning aerospace vehicle dynamics has had far-reaching implications in terms of performance, safety, and operational cost effectiveness. This collection of papers covers a wide range of pertinent topics, including mathematical modelling, computational methods, computer simulation, and developments in control systems. This interesting and timely collection will be of interest to students, engineers, and researchers in applied mathematics and aerospace engineering.
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achieved aerodynamic aeroelastic Aerospace aircraft model algorithm amplitude analysis angle applied approach axis bandwidth blade closed loop coefficients comet comet nucleus control design control law coprime cost function damping damping ratio domain dynamics effects elementary signals equations of motion error failure feedback control Figure filter flight control systems flight dynamics flight test flight vehicle handling qualities helicopter high frequency IEEE implemented information matrix input signals iteration limit cycle linear longitudinal loop controller loop-shaping low frequencies manoeuvres mathematical model measurements method modal model following modes multivariable neural networks nonlinear nutation obtained orbit output parameter estimation performance phase pilot plant problem procedure rad/s real-time reconfiguration response robustness roll rotation rotor rotorcraft sensor sideslip simulation SISO spacecraft speed stability Stengel step responses stepwise regression structure system identification techniques tether thrust vector torque transfer function values variables vector velocity weighting functions wind tunnel zero