Quarternion feedback regulator for spacecraft eigenaxis rotations
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[1] Bong Wie,et al. A new approach to the space-axis rotation , 1987 .
[2] D. C. Redding,et al. Optimized rotation-axis attitude maneuver controller for the Space Shuttle Orbiter , 1987 .
[3] P. P. J. van den Bosch,et al. Adaptive attitude control for large-angle slew manoeuvres , 1986, Autom..
[4] S. Vadali. Variable-Structure Control of Spacecraft Large-Angle Maneuvers , 1986 .
[5] T. A. W. Dwyer,et al. Exact nonlinear control of spacecraft slewing maneuvers with internal momentum transfer , 1984 .
[6] Bong Wie,et al. Quaternion feedback for spacecraft large angle maneuvers , 1984 .
[7] Robin B. Miller. A new strapdown attitude algorithm , 1983 .
[8] R. Mckern,et al. Strapdown Attitude Algorithms from a Geometric Viewpoint , 1981 .
[9] L. D'Amario,et al. A New Single-Rotation-Axis Autopilot for Rapid Spacecraft Attitude Maneuvers , 1979 .
[10] T. Kane. Solution of Kinematical Differential Equations for a Rigid Body , 1973 .
[11] J. Hrastar,et al. Attitude control of a spacecraft with a strapdown inertial reference system and onboard computer , 1970 .
[12] R. Mortensen. A globally stable linear attitude regulator , 1968 .
[13] B. P. Ickes,et al. A new method for performing digital control system attitude computations using quaternions , 1968 .
[14] C. Harding. Solution to Euler’s Gyrodynamics—I , 1964 .
[15] Robert H. Cannon,et al. GYROSCOPIC COUPLING IN SPACE VEHICLE ATTITUDE CONTROL SYSTEMS , 1962 .
[16] R. E. Kalman,et al. Control System Analysis and Design Via the “Second Method” of Lyapunov: I—Continuous-Time Systems , 1960 .
[17] A. C. Robinson,et al. ON THE USE OF QUATERNIONS IN SIMULATION OF RIGID-BODY MOTION , 1958 .
[18] S. V. Salehi,et al. A non-linear feedback attitude regulator† , 1985 .
[19] W. Breckenridge,et al. Quaternions for Galileo scan platform control , 1984 .
[20] C. K. CARRINGTON,et al. Optimal nonlinear feedback control for spacecraft attitude maneuvers , 1983 .
[21] R. A. Mayo. Relative Quaternion State Transition Relation , 1979 .
[22] J. E. Cochran,et al. Adaptive spacecraft attitude control utilizing eigenaxis rotations , 1975 .