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 /
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| Imprint: | Oxford : Clarendon Press ; New York : Oxford University Press, 1994. |
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| Description: | x, 438 p. : ill. ; 24 cm. |
| Language: | English |
| Series: | Institute of Mathematics and Its Applications conference series 47. |
| Subject: | |
| Format: | Print Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/1599391 |
Table of Contents:
- Aerospace vehicle modelling requirements for high bandwidth flight control
- Intelligent flight control systems
- Flight controller design using multivariable loop shaping
- Comparison of LQG, Hoo and classical designs for the pitch rate control of an unstable military aircraft
- A reconfiguration algorithm for real-time aircraft flight control systems
- An analytical redundancy scheme for an automatic flight control system
- Advanced control of high performance rotorcraft
- Design and handling qualities analysis of a full envelope multivariable controller for a combat rotorcraft
- Helicopter flight control design: multivariable methods and design issues
- An investigation into the phenomenon of helicopter blade sailing
- The flight dynamics of an unstable unmanned aircraft
- Recent developments in aircraft parameter identification at Delft University of Technology - optimal input design
- On the use of a modified stepwise regression method to estimate aircraft stability derivatives from dynamic wind tunnel test data
- The performance of CLOS missile systems against weaving targets
- The aeroelastic behaviour of a missile control fin with a pneumatic actuation system
- Navigation in the vicinity of a comet
- Development of a new model with lumped elements for simulation of tethered systems
- Proof-mass actuator control of shuttle based astromast
- Dynamics of a spinning spacecraft containing liquid propellant
