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Advances in Flight Control Systems by Agneta Balint (Ed)

By Agneta Balint (Ed)

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Modeling, Design and Testing of a Barrel-Launched Adaptive Munition," proceedings of the 4" Annual SPIE Symposium on Smart Structures and Materials, San Diego, CA, 3-6 March 1997. , Niceville, Florida, 1993. [30] Hertlein, Robert and Mark Miner, “Extended Range Guided Munition (ERGM) Safe and Arm Device and Height-of-Burst Sensor,” paper presented at the NDIA Fuse Conference, 9 April 2993, New Orleans, LA. pdf [31] Pike, J. org, Alexandria, Virginia, October, 2002. htm). , “M732A2 Proximity Fuse and M782 Multi-Option Fuse for Artillery (MOFA) Data Sheets,” published by Alliant Techsystems, Inc.

The aerodynamic model identification process including the B-spline neural networks is discussed in Sec. IV. Section V validates the performance of the control laws using numerical simulations performed in MATLAB/Simulink. A summary of the results and the conclusions are given in Sec. VI. Finally, an appendix on the concept of constrained adaptive backstepping is included. 2. , 1979). 6 for the wide range of -20 deg ≤ α ≤ 90 deg and -30 deg ≤ β ≤ 30 deg. The control inputs of the model are the elevator, ailerons, rudder, and leading-edge flaps, as well as the throttle setting.

And Weisshaar, T. , "Static Aeroelastic Behavior of an Adaptive Laminated Piezoelectric Composite Wing," AIAA-90-1078-CP, April, 1990, pp. 1611-1623. Adaptive Fight Control Actuators and Mechanisms for Missiles, Munitions and Uninhabited Aerial Vehicles (UAVs) 19 [10] Ehlers, S. , "Adaptive Wing Flexural Axis Control," paper presented at the Third International Conference on Adaptive Structures, sponsored by the ASME, 9 - 11 November, 1992, San Diego. [11] Ehlers, S. , and Weisshaar, T. , "Effect of Material Properties on Static Aeroelastic Control," paper presented at the 33rd Structures, Structural Dynamics and Materials Conference, Dallas, Texas, 15 April, 1992.

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