JPS6431211A - Position control device - Google Patents

Position control device

Info

Publication number
JPS6431211A
JPS6431211A JP62186742A JP18674287A JPS6431211A JP S6431211 A JPS6431211 A JP S6431211A JP 62186742 A JP62186742 A JP 62186742A JP 18674287 A JP18674287 A JP 18674287A JP S6431211 A JPS6431211 A JP S6431211A
Authority
JP
Japan
Prior art keywords
freedom
information
degree
rigidity
degrees
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP62186742A
Other languages
Japanese (ja)
Inventor
Tamane Ozawa
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Corp
Original Assignee
Toshiba Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toshiba Corp filed Critical Toshiba Corp
Priority to JP62186742A priority Critical patent/JPS6431211A/en
Publication of JPS6431211A publication Critical patent/JPS6431211A/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position Or Direction (AREA)

Abstract

PURPOSE:To obtain a vibration-damping effect by regarding the information of a displacement sensor as information obtained in each degree of freedom, applying the rigidity of respectively different frequency characteristics to the information and distributing a control signal to respective driving means by a signal conversion means. CONSTITUTION:Frequency characteristics setting circuits by degree of freedom 341-346 set up frequency characteristics in each degree of freedom. Namely, the gain of rigidity in parallel 3 degrees of freedom is dropped from a comparatively low frequency on a frequency axis and the gain of rigidity in rotational 3 degrees freedom is secured up to a sufficiently high frequency. In a system, respective electromagnets 11... relate to plural degrees of freedom, signals 411-419 from the deformation sensors 21... include plural information of the degree of freedom in a rectangular system and the information of the deformation sensors 21... is converted into signals 431-436 in 6 deg. of freedom. Then, a high frequency component about the displacement of 3 deg. of freedom is removed and converted into driving signals 481-489 obtained in each electromagnet 11.... Consequently position and posture control can be attained without being influenced by the fine oscillation of the structure body.
JP62186742A 1987-07-28 1987-07-28 Position control device Pending JPS6431211A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62186742A JPS6431211A (en) 1987-07-28 1987-07-28 Position control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62186742A JPS6431211A (en) 1987-07-28 1987-07-28 Position control device

Publications (1)

Publication Number Publication Date
JPS6431211A true JPS6431211A (en) 1989-02-01

Family

ID=16193856

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62186742A Pending JPS6431211A (en) 1987-07-28 1987-07-28 Position control device

Country Status (1)

Country Link
JP (1) JPS6431211A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5226099A (en) * 1991-04-26 1993-07-06 Texas Instruments Incorporated Digital micromirror shutter device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5226099A (en) * 1991-04-26 1993-07-06 Texas Instruments Incorporated Digital micromirror shutter device

Similar Documents

Publication Publication Date Title
EP0845676A3 (en) Triaxial angular rate and acceleration sensor
EP0371344A3 (en) Stabilization of a spinning spacecraft of arbitrary shape
JP2002523291A5 (en)
GB8610800D0 (en) Resultant velocity control
JPS6431211A (en) Position control device
EP0067880A4 (en) Robot control system.
CA2095033A1 (en) Active Vibration Control System
CA2028371A1 (en) Suspension control apparatus
GB8917223D0 (en) Attitude sensor
VORONIN A self-tunable system with a reference model for the control of a robotic manipulator(Samonastraivaiushchaiasia sistema s etalonnoi model'iu dlia upravleniia manipuliatsionnym robotom)
JPS55142231A (en) Rotation controller for vibrating table
JPS6447699A (en) Attitude controller for artificial satellite
JPH0437838Y2 (en)
CA2001199A1 (en) Signal processing means for identifying systems subject to periodic disturbances
JPS62134693U (en)
Kashiwase et al. Attitude control for flexible space structures with loose couplers.
JPS6180200U (en)
JPS6435404U (en)
IGONIN et al. Increasing the accuracy of state-vector estimation under conditions of the incomplete observability of an extended system((for spacecraft motion control system synthesis))(Povyshenie tochnosti otsenki vektora sostoianiia v usloviiakh nepolnoi nabliudaemosti rasshirennoi sistemy)
CROWLEY Dynamic world modeling for an intelligent mobile robot using a rotating ultra-sonic ranging device[Interim Report]
JPS63148099U (en)
JPH0190699U (en)
JPS63602U (en)
JPH0413665U (en)
JPS6242319U (en)