- 专利标题: Rotary wing aircraft vibration control system with resonant inertial actuators
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申请号: US13983463申请日: 2012-02-03
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公开(公告)号: US10308354B2公开(公告)日: 2019-06-04
- 发明人: Paul Black , Doug Swanson , Askari Badre-Alam , David Edeal , Douglas Pedersen
- 申请人: Paul Black , Doug Swanson , Askari Badre-Alam , David Edeal , Douglas Pedersen
- 申请人地址: US NC Cary
- 专利权人: LORD Corporation
- 当前专利权人: LORD Corporation
- 当前专利权人地址: US NC Cary
- 国际申请: PCT/US2012/023802 WO 20120203
- 国际公布: WO2012/106616 WO 20120809
- 主分类号: G01C23/00
- IPC分类号: G01C23/00 ; G05D1/00 ; G05D3/00 ; G06F7/00 ; G06F17/00 ; B64C27/00 ; F16F7/10 ; H02K33/00 ; H02P25/032
摘要:
A control system for resonant inertial actuators estimates operating parameters of the resonant inertial actuators based on voltage and current feedback and dynamically limits selected parameters to maintain the safe, efficient, and cost effective operation of the resonant inertial actuators. Resistance within the electrical drives for the resonant inertial actuators is estimated from the voltage and current feedback and in conjunction with the modeling of the resonant inertial actuators other operating parameters are calculated or otherwise estimated. Having regard for the responsiveness of the resonant inertial actuators to changes in command signals, the command signals are adjusted to dynamically limit the estimated parameters.
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