Fourier-based optimal design of a flexible manipulator path to reduce residual vibration of the endpoint

[1]  P. H. Meckl,et al.  Minimizing Residual Vibration for Point-to-Point Motion , 1985 .

[2]  C. Swigert Shaped Torque Techniques , 1980 .

[3]  Wayne J. Book,et al.  Experiments in optimal control of a flexible arm , 1985 .

[4]  A. Akay,et al.  Vibration reduction of a flexible arm by time-optimal open-loop control , 1991 .

[5]  H. Tokumaru,et al.  Inverse Dynamics of Flexible Robot Arms: Modeling and Computation for Trajectory Control , 1990 .

[6]  James D. Turner,et al.  Optimal distributed control of a flexible spacecraft during a large-angle maneuver , 1984 .

[7]  K. Tompetrini,et al.  Space telescope pointing control system , 1982 .

[8]  R. L. Farrenkopf Optimal Open-Loop Maneuver Profiles for Flexible Spacecraft , 1979 .

[9]  Warren P. Seering,et al.  Preshaping Command Inputs to Reduce System Vibration , 1990 .

[10]  R. H. Cannon,et al.  Initial Experiments on the End-Point Control of a Flexible One-Link Robot , 1984 .

[11]  S. Choura,et al.  On the finite settling time and residual vibration control of flexible structures , 1991 .

[12]  C. S. G. Lee,et al.  Robotics: Control, Sensing, Vision, and Intelligence , 1987 .

[13]  J. A. Breakwell,et al.  Optimal feedback slewing of flexible spacecraft , 1981 .

[14]  Larry Silverberg Uniform damping control of spacecraft , 1986 .

[15]  J. R Hewit,et al.  Optimal trajectory control of robotic manipulators , 1984 .

[16]  P. H. Meckl,et al.  Active Damping in a Three-Axis Robotic Manipulator , 1985 .

[17]  D. M. Aspinwall Acceleration Profiles for Minimizing Residual Response , 1979 .

[18]  J. Junkins,et al.  Optimal Large-Angle Single-Axis Rotational Maneuvers of Flexible Spacecraft , 1980 .