Controller Design for D-SEND#2
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/64/3/64_64_160/_pdf
Reference9 articles.
1. 2) Meyer, G., Su, R. and Hunt, L. R.: Application of Nonlinear Transformations to Automatic Flight Control, Automatica, 20 (1984), pp. 103-107.
2. 3) Lane, S. H. and Stengel, R. F.: Flight Control Design Using Non-linear Inverse Dynamics, Automatica, 24 (1988), pp. 471-483.
3. 4) Enns, D., Bugajski, D., Hendrick, R. and Stein, G.: Dynamic Inversion: An Evolving Methodology for Flight Control Design, Int. J. Control, 59 (2007), pp. 71-91.
4. 5) Prasad, J. V. R., Calise, A. J., Pei, Y. and Corban, J. E.: Adaptive Nonlinear Controller Synthesis and Flight Test Evaluation on an Unmanned Helicopter, Proc. of the 1999 IEEE International Conference on Control Applications, Vol. 1, 1999, pp. 137-142.
5. 6) Menon, P. K. A., Iragavarapu, V. R. and Ohlmeyer, E. J.: Nonlinear Missile Autopilot Design Using Time-Scale Separation, AIAA Guidance, Navigation and Control Conference, AIAA Paper 97-3765, 1997.
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