Robust Nonlinear Spacecraft Attitude Control using Incremental Nonlinear Dynamic Inversion.

[1]  Gertjan Looye An Integrated Approach to Aircraft Modelling and Flight Control Law Design , 2008 .

[2]  Suresh M. Joshi,et al.  Reconfigurable NDI controller using inertial sensor failure detection & isolation , 2001 .

[3]  Jan Albert Mulder,et al.  Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction , 2010 .

[4]  Aaron J. Ostroff,et al.  RECONFIGURABLE FLIGHT CONTROL USING NONLINEAR DYNAMIC INVERSION WITH A SPECIAL ACCELEROMETER IMPLEMENTATION , 2000 .

[5]  Gary J. Balas,et al.  Flight control design using robust dynamic inversion and time-scale separation , 1996, Autom..

[6]  P. Tsiotras Stabilization and optimality results for the attitude control problem , 1996 .

[7]  Bong Wie,et al.  Rapid Multitarget Acquisition and Pointing Control of Agile Spacecraft , 2000 .

[8]  Jan Albert Mulder,et al.  Reentry Flight Controller Design Using Nonlinear Dynamic Inversion , 2003 .

[9]  S. Juliana Re-entry flight clearance , 2006 .

[10]  Roger W. Brockett,et al.  Feedback Invariants for Nonlinear Systems , 1978 .

[11]  W. F. Phillips,et al.  Review of Attitude Representations Used for Aircraft Kinematics , 2001 .

[12]  Shunan Wu,et al.  Quaternion-based finite time control for spacecraft attitude tracking , 2011 .

[13]  M. Shuster A survey of attitude representation , 1993 .

[14]  P R Smith,et al.  A SIMPLIFIED APPROACH TO NONLINEAR DYNAMIC INVERSION BASED FLIGHT CONTROL , 1998 .

[15]  Arthur J. Krener,et al.  A Decomposition Theory for Differentiable Systems , 1975 .