By Agneta Balint (Ed)
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Extra resources for Advances in Flight Control Systems
1217 - 1219.  Barrett, R. , Techno House, Bristol, UK, Vol. 5, No. 2, March 1996, pp. 121-128. , "Active Aeroelastic Tailoring of an Adaptive Flexspar Stabilator," Journal of Smart Materials and Structures, Vol. 5, No. 6 December 1996, Techno House, Bristol, UK, 1996, pp. 723 – 730. , “Design, Construction and Testing of a Proof-of-Concept Smart Compressed Reversed Adaptive Munition,” Final Report to the USAF Armament Directorate, Wright Laboratory, Eglin AFB, FL contract no. AF-FO863095-K-0079, September, 1996.
The number and size of the hyperboxes should be based on a priori information on the physical properties of the vehicle on hand, and may be defined in terms of state variables as Mach number, angle of attack and engine thrust. , 2003) to interpolate between the local models to ensure smooth model transitions. Numerical simulations of various maneuvers with aerodynamic uncertainties in the model and actuator failures are presented. The maneuvers are performed at several flight conditions to demonstrate that the control laws are valid for the entire flight envelope.
October 2008. , "Dynamic Elastic Axis Shifting: An Important Enhancement of Piezoelectric Postbuckled Precompressed Actuators," The Journal of the American Institute of Aeronautics and Astronautics, Vol. 48, No. 3 March 2010. , "Hypermaneuverability and Visual Cloaking; New Adaptive Aerostructures Technologies for Uninhabited Aerial Vehicles (UAVs)," The Aeronautical Journal, Royal Aeronautical Society, London, UK, Vol. 114, No. 1156, June 2010. , "Post-Buckled Precompressed Techniques In Adaptive Aerostructures: An Overview," MD-08-1306 Journal of Mechanical Design, Vol.