Vehicle attitude control using finite time convergence incremental nonlinear dynamic inversion combined the command differential signals
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[1] Daniel J. Bugajski,et al. A dynamic inversion based control law with application to the high angle-of-attack research vehicle , 1990 .
[2] Anthony J. Calise,et al. Nonlinear flight control using neural networks , 1994 .
[3] I. Craig,et al. Robust flight controller design using H-infinity loop-shaping and dynamic inversion techniques , 1998 .
[4] Chen Zhi-xiang. Design of Incremental Dynamic Inversion Control Law for Missiles with Tracking Differentiator , 2012 .
[5] P R Smith,et al. A SIMPLIFIED APPROACH TO NONLINEAR DYNAMIC INVERSION BASED FLIGHT CONTROL , 1998 .
[6] Zhang Ju. Control Law Design of Hypersonic Vehicle Based on Incremental Dynamic Inverse , 2013 .
[7] Jan Albert Mulder,et al. Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction , 2010 .
[8] Wen-Hua Chen,et al. Nonlinear Disturbance Observer-Enhanced Dynamic Inversion Control of Missiles , 2003 .
[9] Massimiliano Mattei,et al. Incremental Nonlinear Dynamic Inversion and Control Allocation for a Tilt Rotor UAV , 2014 .
[10] Ji-hua Zhou,et al. Marker-Assisted Selection for Stv-b i Gene Controlling Resistance to Rice Stripe Disease: Marker-Assisted Selection for Stv-b i Gene Controlling Resistance to Rice Stripe Disease , 2009 .