Flight test of an adaptive control system for unmanned helicopter trajectory following
暂无分享，去创建一个
[1] J. V. R. Prasad,et al. Synthesis of a helicopter nonlinear flight controller using approximate model inversion , 1993 .
[2] Anthony J. Calise,et al. Implementation of adaptive nonlinear control for flight test on an unmanned helicopter , 1998, Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171).
[3] Anthony J. Calise,et al. Nonlinear adaptive flight control using neural networks , 1998 .
[4] Kevin A. Wise,et al. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft , 2000 .
[5] Eric N. Johnson,et al. FEEDBACK LINEARIZATION WITH NEURAL NETWORK AUGMENTATION APPLIED TO X-33 ATTITUDE CONTROL , 2000 .
[6] Anthony J. Calise,et al. Adaptive nonlinear controller synthesis and flight test evaluation on an unmanned helicopter , 1999, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328).
[7] Anthony J. Calise,et al. High Bandwidth Adaptive Flight Control , 2000 .
[8] Anthony J. Calise,et al. Application of an Adaptive Autopilot Design to a Family of Guided Munitions , 2000 .
[9] Seungjae Lee,et al. Direct adaptive reconfigurable control of a tailless fighter aircraft , 1998 .