Patent US4467186A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4467186A Expired / Lapsed US ⏱️ 0.0 years remaining

Mirror actuator control system

Assignee: United States Department of the Air Force
•
Filing: 1982-01-27
•
Granted: 1984-08-21
•
Expires: 2002-01-27
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A mirror actuator control system utilizing a wavefront sensor to determine the resulting angle error signal between the wavefront tilt angle and the mirror tilt angle. The resulting angle error signal is used to drive the actuator unit which controls the mirror tilt angle.

Inventors

  • 👤 Norman S. Goralnick
  • 👤 George H. McLellan, Jr.

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 20:42
CPC Classifications
G; G01; G01J; G01J9/00; G01S; G01S17/00; G01S17/66; G02; G02B; G02B26/00; G02B26/06

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 218 words
A mirror actuator control system comprising in combination: means for sensing a wavefront tilt angle, said wavefront tilt angle sensing means providing a wavefront tilt angle signal, means for sensing a mirror tilt angle, said mirror tilt angle sensing means providing a mirror tilt angle signal, means for comparing said wavefront tilt angle signal with said mirror tilt angle signal, said comparing means providing a tilt error signal, a wavefront sensor means sampling and quantizing said tilt error signal, said wavefront sensor means providing a tilt correction signal, a gain unit having a predetermined gain factor, said gain unit amplifying said tilt correction signal by said gain factor; a compensation network receiving said tilt correlator signal, said compensation network maintaining the signal level with a predetermined range, said compensation network compensating for the mechanical system natural frequency, said compensation network reducing the high frequency noise in said tilt correction signal, said compensation network providing an output signal, a drive amplifier receiving the output signal from said compensation network, said drive amplifier having a correct gain to provide a lag beyond the loop crossover frequency, said drive amplifier providing a current signal, and, an actuator means receiving said current signal and providing a torque in response thereto, said torque being applied to a mirror to change its tilt angle.
Claim 2
Dependent Claim 218 words
A mirror actuator control system comprising in combination: means for sensing a wavefront tilt angle, said wavefront tilt angle sensing means providing a wavefront tilt angle signal, means for sensing a mirror tilt angle, said mirror tilt angle sensing means providing a mirror tilt angle signal, means for comparing said wavefront tilt angle signal with said mirror tilt angle signal, said comparing means providing a tilt error signal, a wavefront sensor means sampling and quantizing said tilt error signal, said wavefront sensor means providing a tilt correction signal, a gain unit having a predetermined gain factor, said gain unit amplifying said tilt correction signal by said gain factor; a compensation network receiving said tilt correlator signal, said compensation network maintaining the signal level with a predetermined range, said compensation network compensating for the mechanical system natural frequency, said compensation network reducing the high frequency noise in said tilt correction signal, said compensation network providing an output signal, a drive amplifier receiving the output signal from said compensation network, said drive amplifier having a correct gain to provide a lag beyond the loop crossover frequency, said drive amplifier providing a current signal, and, an actuator means receiving said current signal and providing a torque in response thereto, said torque being applied to a mirror to change its tilt angle.
Claim 3
Dependent Claim 46 words
A mirror actuator control system as described in claim 1 wherein said wavefront sensor means comprises a sample and hold means to sample said tilt error signal, and, a quantizer means to process said tilt error signal into one of a finite number of 256 subranges.
Claim 4
Dependent Claim 17 words
A mirror actuator control system as described in claim 1 wherein said gain factor is 9070 volts/radian.
Claim 5
Dependent Claim 18 words
A mirror actuator control system as described in claim 1 wherein said drive amplifier comprises a current amplifier.
Claim 6
Dependent Claim 23 words
A mirror actuator control system as described in claim 1 wherein said compensation means comprises an integrator and a double lead lag network.
Claim 7
Dependent Claim 100 words
A mirror actuator control system as described in claim 1 wherein said actuator means comprises in combination: a pair of drive units to respond to said current signal, an actuator housing to support said pair of drive units, a flexible pivot means attached to said actuator housing, a bezel means supported by said flexible pivot means and said pair of drive units, said bezel means fixedly attached to said flexible pivot means, and, a mirror attached to said bezel means, said mirror having a hole passing through the center thereof, said hole extending through said bezel and said actuator housing.
Claim 8
Dependent Claim 17 words
A mirror actuator control system as described in claim 2 wherein said sampling time is 100 microseconds.
Claim 9
Dependent Claim 19 words
A mirror actuator control system as described in claim 2 wherein said finite number of subranges is 8 bits.
Claim 10
Dependent Claim 21 words
A mirror actuator control system as described in claim 4 wherein said current amplifier is a power amplifier with current feedback.
Claim 11
Dependent Claim 18 words
A mirror actuator control system as described in claim 7 wherein the least significant bit equals 0.15 microradians.

References Cited (Backward Citations)

US3708736A Cited
US4326800A Cited
US4399356A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-08-21 1988-02-20 1988-08-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-08-21 1992-02-20 1992-08-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-08-21 1996-02-20 1996-08-21 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag