Title :
Frequency-weighting filter selection for H2 control of microgravity isolation systems: A consideration of the “implicit frequency weighting” problem
Author :
Hampton, R. David ; Whorton, Mark S.
Author_Institution :
MAE Dept., Alabama Univ., Huntsville, AL, USA
fDate :
4/1/2000 12:00:00 AM
Abstract :
Many space-science experiments need an active isolation system to provide them with the requisite microgravity environment. The isolation systems planned for use with the International Space Station (ISS) have been appropriately modeled using relative position, relative velocity, and acceleration states. In theory, frequency-weighting design filters can be applied to these state-space models, in order to develop optimal H2 or mixed-norm controllers with desired stability and performance characteristics. In practice, however, since there is a kinematic relationship among the various states, any frequency weighting applied to one state will implicitly weight other states. These implicit frequency-weighting effects must be considered, for intelligent frequency-weighting filter assignment. This paper suggests a rational approach to the assignment of frequency-weighting design filters, in the presence of the kinematic coupling among states that exists in the microgravity vibration isolation problem
Keywords :
aerospace control; circuit feedback; continuous time systems; filters; network synthesis; optimal control; vibration isolation; zero gravity experiments; H2 control; International Space Station; active isolation; continuous time system; feedback; frequency-weighting effects; frequency-weighting filter selection; implicit frequency weighting; intelligent frequency-weighting filter; kinematic coupling; microgravity environment; microgravity isolation; microgravity vibration isolation; mixed-norm controllers; optimal H2; optimal control; performance characteristics; space-science experiments; stability; state-space models; Acceleration; Control systems; Filters; Frequency; Hydrogen; Isolation technology; Isolators; Optimal control; Payloads; Space technology;
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on