Control of the F-14 Aircraft Lateral-Directional Axis during Powered Approach
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Control of the F-14 Aircraft Lateral-Directional Axis during Powered Approach
Published Date
1998
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American Institute of Aeronautics and Astronautics
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Article
Abstract
The design of linear controllers for the F-14 aircraft lateral-directional axis during powered approach using the structured singular-value (μ) framework is presented. Controllers are designed for an angle of attack of 10.5 deg and an airspeed of 137 kn, the on-speed flight condition. Each controller is implemented in a simplified nonlinear simulation and the full-order Fortran nonlinear simulation of the F-14. Pilot-in-the-loop simulations are used to verify their performance in the crewed flight simulator at the U.S. Naval Air Warfare Center, Patuxent River, Maryland. The μ controllers out perform the current analog and newly developed digital lateral-directional powered approach flight control system in pilot-in-the-loop simulations.
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Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http://www.aiaa.org/content.cfm?pageid=2 for more information.
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Previously Published Citation
Balas, G. J., Packard, A. K., Renfrow, J., Mullaney, C., and M'Closkey, R. T. (1998). "Control of the F-14 Aircraft Lateral-Directional Axis during Powered Approach." Journal of Guidance, Control, and Dynamics. 21(6), 899-908.
Suggested citation
Balas, Gary J.; Packard, Andrew K.; Renfrow, Joseph; Mullaney, Chris; M'Closkey, Robert T.. (1998). Control of the F-14 Aircraft Lateral-Directional Axis during Powered Approach. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/37124.
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