Tensor Product Model-Based Gain Scheduling of a Missile Autopilot
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/59/3/59_T-15-19/_pdf
Reference26 articles.
1. 1) Rugh, W. J. and Shamma, J. S.: Research on Gain Scheduling, Automatica, 36 (2000), pp. 1401–1425.
2. 2) Shamma, J. S. and Cloutier, J. R.: Gain-scheduled Missile Autopilot Design using Linear Parameter Varying Transformations, J. Guid. Control Dynam., 16 (1993), pp. 256–263.
3. 3) Pellanda, P. C., Apkarian, P., and Tuan, H. D.: Missile Autopilot Design via a Multi-channel LFT/LPV Control Method, Int. J. Robust Nonlin., 12 (2002), pp. 1–20.
4. 4) Wu, F., Packard, A., and Balas, G.: Systematic Gain-Scheduling Control Design: A Missile Autopilot Example, Asian J. Contro., 4 (2002), pp. 341–347.
5. 5) Stilwell, D. J.: State-space Interpolation for a Gain-scheduled Autopilot, J. Guid. Control Dynam., 24 (2001), pp. 460–465.
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