NEAR-OPTIMAL FEEDBACK GUIDANCE FOR AN ACCURATE LUNAR LANDING

[1]  D. Doman,et al.  Trajectory generation using a modified simple shooting method , 2004, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).

[2]  David B. Doman,et al.  A modified simple shooting method for solving two-point boundary-value problems , 2003, 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652).

[3]  Tayfun Çimen,et al.  State-Dependent Riccati Equation (SDRE) Control: A Survey , 2008 .

[4]  Harvey Thomas Banks,et al.  Feedback Control Methodologies for Nonlinear Systems , 2000 .

[5]  Robert C. Nelson,et al.  Flight Stability and Automatic Control , 1989 .

[6]  Robert H. Bishop,et al.  Enhanced Apollo Targeting for Lunar Landing , 2008 .

[7]  Christina Tvrdik Chomel.  Development of an analytical guidance algorithm for lunar descent , 2007 .

[8]  Anil V. Rao,et al.  Practical Methods for Optimal Control Using Nonlinear Programming , 1987 .

[9]  Frank L. Lewis,et al.  Aircraft Control and Simulation , 1992 .

[10]  Mario Innocenti,et al.  Estimation of the Region of Attraction for State-Dependent Riccati Equation Controllers , 2006 .

[11]  Jeff S. Shamma,et al.  Existence of SDRE stabilizing feedback , 2003, IEEE Trans. Autom. Control..

[12]  Panagiotis Tsiotras,et al.  A State-Dependent Riccati Equation Approach to Atmospheric Entry Guidance , 2010 .

[13]  Victor M. Becerra,et al.  Optimal control , 2008, Scholarpedia.

[14]  D. Geller,et al.  Terrain-Relative and Beacon-Relative Navigation for Lunar Powered Descent and Landing , 2011 .

[15]  J. Cloutier,et al.  Control designs for the nonlinear benchmark problem via the state-dependent Riccati equation method , 1998 .

[16]  H. T. Banks,et al.  Nonlinear feedback controllers and compensators: a state-dependent Riccati equation approach , 2007, Comput. Optim. Appl..

[17]  Zdzislaw Bubnicki,et al.  Modern Control Theory , 2005 .

[18]  J. Cloutier.  State-dependent Riccati equation techniques: an overview , 1997, Proceedings of the 1997 American Control Conference (Cat. No.97CH36041).

[19]  Robert H. Bishop,et al.  Analytical Lunar Descent Guidance Algorithm , 2009 .

[20]  Ronald R. Sostaric.  Powered Descent Trajectory Guidance and Some Considerations for Human Lunar Landing , 2007 .

[21]  J. R. Cloutier,et al.  The capabilities and art of state-dependent Riccati equation-based design , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

[22]  Howard D. Curtis,et al.  Orbital Mechanics for Engineering Students , 2005 .

[23]  Yuhong Zhang,et al.  Optimal control using state dependent riccati equation (SDRE) for a flexible cable transporter system with arbitrarily varying lengths , 2005, Proceedings of 2005 IEEE Conference on Control Applications, 2005. CCA 2005..

[24]  S. C. Beeler,et al.  State Estimation and Tracking Control of Nonlinear Dynamical Systems , 2003 .

[25]  David B. Doman,et al.  Combining State Dependent Riccati Equation Approach With Dynamic Inversion: Application to Control of Flight Vehicles , 2003 .

[26]  Allan R. Klumpp,et al.  Apollo lunar descent guidance , 1974, Autom..

[27]  P. K. Menon,et al.  Real-time computational methods for SDRE nonlinear control of missiles , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

[28]  J. R. Cloutier,et al.  Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method , 1994 .

[29]  Stephen P. Banks,et al.  Global optimal feedback control for general nonlinear systems with nonquadratic performance criteria , 2004, Syst. Control. Lett..

[30]  F. Bennett.  Apollo experience report: Mission planning for lunar module descent and ascent , 1972 .

[31]  J. Guo,et al.  DESIGN OF GUIDANCE LAWS FOR LUNAR PINPOINT SOFT LANDING , 2009 .

[32]  Stephen P. Banks,et al.  Nonlinear optimal tracking control with application to super-tankers for autopilot design , 2004, Autom..

[33]  George M. Siouris,et al.  Applied Optimal Control: Optimization, Estimation, and Control , 1979, IEEE Transactions on Systems, Man, and Cybernetics.