Dynamic modeling and ascent flight control of Ares-I Crew Launch Vehicle

[1]  R. Clough,et al.  Dynamics Of Structures , 1975 .

[2]  Stephan R. Davis,et al.  Ares I-X Flight Test--The Future Begins Here , 2008 .

[3]  Roy S. Smith,et al.  The design of H∞ controllers for an experimental non-collocated flexible structure problem , 1994, IEEE Trans. Control. Syst. Technol..

[4]  Haim Weiss,et al.  Quarternion feedback regulator for spacecraft eigenaxis rotations , 1989 .

[5]  Cornelius T. Leondes,et al.  Guidance and control of aerospace vehicles , 1963 .

[6]  Gene F. Franklin,et al.  Feedback Control of Dynamic Systems , 1986 .

[7]  Bong Wie,et al.  New generalized structural filtering concept for active vibration control synthesis , 1989 .

[8]  Bong Wie,et al.  Space Vehicle Dynamics and Control , 1998 .

[9]  Panagiotis Tsiotras,et al.  Spin-axis stabilization of symmetric spacecraft with two control torques , 1994 .

[10]  James Frosch,et al.  Saturn AS-501/S-IC flight control system design. , 1967 .

[11]  Rajesh Rajamani,et al.  Vehicle dynamics and control , 2005 .

[12]  Ian Postlethwaite,et al.  Multivariable Feedback Control: Analysis and Design , 1996 .

[13]  H. Krishnan,et al.  Attitude stabilization of a rigid spacecraft using gas jet actuators operating in a failure mode , 1992, [1992] Proceedings of the 31st IEEE Conference on Decision and Control.

[14]  Stephen A. Cook,et al.  Ascent Flight Control and Structural Interaction for the Ares-I Crew Launch Vehicle , 2007 .

[15]  Gary J. Balas,et al.  Control of lightly damped, flexible modes in the controller crossover region , 1994 .

[16]  J. Doyle,et al.  Robust and optimal control , 1995, Proceedings of 35th IEEE Conference on Decision and Control.

[17]  Russell Sievers,et al.  Saturn V guidance, navigation, and targeting. , 1967 .

[18]  M. H. Rheinfurth The alleviation of aerodynamic loads on rigid space vehicles , 1966 .

[19]  Greg Dukeman,et al.  Rapid Trajectory Optimization for the ARES I Launch Vehicle , 2008 .

[20]  Bong Wie,et al.  Quaternion feedback for spacecraft large angle maneuvers , 1985 .

[21]  Jay Brandon,et al.  Ares I Flight Control System Overview , 2008 .

[22]  Peter H. Zipfel,et al.  Modeling and Simulation of Aerospace Vehicle Dynamics , 2001 .

[23]  T. Blackburn,et al.  Application of linear optimal control and filtering theory to the Saturn V launch vehicle , 1971 .

[24]  D. Garner Control theory handbook , 1964 .

[25]  S. Sastry Nonlinear Systems: Analysis, Stability, and Control , 1999 .

[26]  Jay M. Brandon,et al.  Ares-I-X Stability and Control Flight Test: Analysis and Plans , 2008 .

[27]  P. Crouch,et al.  Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models , 1984 .

[28]  Bong Wie,et al.  Robust non-minimum-phase compensation for a class of uncertain dynamical systems , 1991 .

[29]  Bruce A. Francis,et al.  Feedback Control Theory , 1992 .

[30]  Matthew Johnson,et al.  Stability Analysis of the NASA ARES I Crew Launch Vehicle Control System , 2007 .

[31]  John H. Blakelock,et al.  Automatic control of aircraft and missiles , 1965 .

[32]  James McDuffie,et al.  Time Domain Simulation of the NASA Crew Launch Vehicle , 2007 .

[33]  Panagiotis Tsiotras,et al.  A novel approach to the attitude control of axisymmetric spacecraft , 1995, Autom..

[34]  Wei Du,et al.  Analysis and Design of Launch Vehicle Flight Control Systems , 2008 .

[35]  Adam Butt,et al.  NASA Ares I Launch Vehicle Roll and Reaction Control Systems Design Status , 2009 .

[36]  Gary J. Balas,et al.  Robustness and performance tradeoffs in control design for flexible structures , 1990, 29th IEEE Conference on Decision and Control.

[37]  Christopher I. Byrnes,et al.  On the attitude stabilization of rigid spacecraft , 1991, Autom..

[38]  Phil Sumrall The Ares Projects: Progress Toward Exploration , 2008 .

[39]  Arthur L. Greensite,et al.  Analysis and design of space vehicle flight control systems , 1970 .