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A Terminal Control Landing System: Theory, System Integration Concepts, and Flight Test Results
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Abstract
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Citation
Farnum, D. and Montooth, J., "A Terminal Control Landing System: Theory, System Integration Concepts, and Flight Test Results," SAE Technical Paper 620539, 1962, https://doi.org/10.4271/620539.Also In
References
- Matthews M. V. Steeg C. W. “Terminal Controller Synthesis,” MIT, 55-272 (Nov. 4, 1955), 10. Presented at Princeton Symposium on Nonlinear Control Systems March 26-27 1956
- Boonton R. C. Jr. “Optimum Design of Final-Value Control Systems.” Proceedings Polytechnic Institute of Brooklyn, Symposium on Nonlinear Control Systems 1956
- Morris R. V. “Design of a Motion Control System Subject to Constraints.” M.S. Thesis, MIT Electrical Engrg. Dept. 1956
- Montooth J. W. “Terminal Control System Synthesis.” Presented to SAE Committee A-18 Washington, D. C June 14-16 1961
- O’Hern E. A. Smyth R. K. “Terminal Control System Application.” Presented at IRE Joint Automatic Control Conference, University of Colorado Boulder, Colo. June 28-30 1961
- Smyth R. K. Velander E. W. “Autoflare Landing System for Jet Transports.” Presented at SAE National Aeronautic Meeting New York April 4-7 1961
- Holm E. R. Proferes N. J. Winick A. B. “Capability of the Directional Localizer as a Source of Guidance for Landing.” Navigation Branch, Bureau of Research and Development Federal Aviation Agency April 7 1961
- Smyth R. K. “Inertial Rate of Descent System.” Proceedings of IRE and ARS Spring Technical Conference Cincinnati April 12-13 1960