Quarternion feedback regulator for spacecraft eigenaxis rotations

[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 .