Command profile for Galileo scan platform controlA recursive command profile is developed for the control of a two-degree-of-freedom scan platform mounted on a flexible structure. Perfect sensors and actuators are assumed for development and testing, and structural vibrations are minimized by actuator torque commands following a smooth torque-time profile. The integral of the smooth torque profile, the rate profile, is recursively generated by a piecewise constant second derivation, and the torque applied by the closk actuator is divided into three components. Results show that the smooth platform motion in response to the command profiles is what the Galileo control systems needs to avoid stator structural vibrations. Position, rate and acceleration profiles are also presented, and the resulting motion of the scan platform in response to command profiles is illustrated.
Document ID
19810061439
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Man, G. K. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Breckenridge, W. G. (California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1981
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 81-190Report Number: AAS PAPER 81-190
Meeting Information
Meeting: Astrodynamics Specialist Conference
Location: Lake Tahoe, NV
Country: US
Start Date: August 3, 1981
End Date: August 5, 1981
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society