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
著者
書誌事項
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
（The Institute of Mathematics and its Applications conference series, new series. 47）
Clarendon Press , Oxford University Press, 1994
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内容説明・目次
内容説明
Rapid developments of computer technology have affected the analysis, synthesis and control of every aspect of aerospace vehicle dynamics. The rewards of increased research have had far reaching implications in terms of performance, safety, and operational cost effectiveness. New challenges have emerged in the wake of the recent shift in emphasis from military to civil applications. This collection of papers covers a wide range of topics including mathematical modelling, computational methods, computer simulation, and developments in control systems. The first paper is on aerospace vehicle modelling requirements for high bandwidth flight control (P.G. Hamel, Braunschweig University, Germany); there is a paper on advanced control of high performance rotocraft (Ian Postlethwaite and D.G. Walker, University of Leicester); a paper on recent developments in aircraft parameter indentification and optimal input design (C.A.A.M. van der Linden, J.A. Mulder and J.K. Sridhar, Delft University of Technology, The Netherlands); a section on intellegent flight control systems (R.F. Stengel, Princeton University, USA); navigation in the vicinity of a comet (M. Noton, British Aerospace, Bristol).
In summary, this is a topical selection of papers on recent research in an area of growing interest and application.
目次
1: P.G. Hamel: Aerospace vehicle modelling requirements for high bandwidth flight control. 2: R.F. Stengel: Intelligent flight control systems. 3: R.A. Hyde and K. Glover: Flight controller design using multivariable loop shaping. 4: S.A. Carr and M.J. Grimble: Comparison of LQG, Hoo and classical designs for the pitch rate control of an unstable military aircraft. 5: F. Caliskan and R. Vepa: A reconfiguration algorithm for real-time aircraft flight control systems. 6: D. McLean and H. Benkhedda: An analytical redundancy scheme for an automatic flight control system. 7: I. Postlethwaite and D.J. Walker: Advanced control of high performance rotorcraft. 8: D. Maclay and J. Howitt: Design and handling qualities analysis of a full envelope multivariable controller for a combat rotorcraft. 9: J.J. Gribble, M.A. Manness and D.J. Murray-Smith: Helicopter flight control design: multivariable methods and design issues. 10: S. Newman: An investigation into the phenomenon of helicopter blade sailing. 11: P.G. Thomasson: The flight dynamics of an unstable unmanned aircraft. 12: C.A.A.M. van der Linden, J.A. Mulder and J.K. Sridhar: Recent developments in aircraft parameter identification at Delft University of Technology - optimal input design. 13: H.A. Hinds and M.V. Cook: On the use of a modified stepwise regression method to estimate aircraft stability derivatives from dynamic wind tunnel test data. 14: D.H. Vorley: The performance of CLOS missile systems against weaving targets. 15: A.P. Lewis: The aeroelastic behaviour of a missile control fin with a pneumatic actuation system. 16: M. Noton: Navigation in the vicinity of a comet. 17: M. Morana: Development of a new model with lumped elements for simulation of tethered systems. 18: C.L. Kirk and M.S. Lee: Proof-mass actuator control of shuttle based astromast. 19: D.G.H. Tan: Dynamics of a spinning spacecraft containing liquid propellant
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