Torque control system for reaction wheel assemblies and the like

• US 3,968,352 A
• Filed: 05/17/1974
• Issued: 07/06/1976
• Est. Priority Date: 05/17/1974
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Sperry Rand Corporation (Unisys Corporation)
• Inventors: Andeen, Richard E.
• Primary Examiner(s): Botz, Eugene G.
• Application Number:
  US05/470,879
• Time in Patent Office: 781 Days
• Field of Search: 318/618, 318/580, 318/582, 318/584, 318/586, 318/566, 318/600, 318/603, 318/604, 235/150.2, 235/150.27, 244/165, 244/170, 74/5.6 R
• US Class Current: 701/13
• CPC Class Codes: B64G 1/283 using reaction wheels
• CPC Class Codes: H02P 23/16 Controlling the angular speed of one shaft H02P23/18 takes precedence
• CPC Class Codes: Y10T 74/1261 with pick off

Abstract

An improvement in torque control systems for reaction wheel assemblies and the like used primarily for stabilizing space vehicles such as satellites including means for integrating the torque command signal and combining the integrated torque command signal with a feedback signal proportional to the angular speed of the rotor of the reaction wheel assembly thereby producing an error signal proportional to the difference between the integrated torque command signal and the angular speed signal. The error signal is coupled to the rotor spin motor which produces a resultant output torque that has been compensated for disturbance torques and other anomalies whereby the resultant torque applied to the rotor and consequently to the satellite is substantially equal to the commanded torque.

Claims

1. A control torque command circuit in a reaction wheel assembly which includes a sensitive element rotating at an angular velocity, ω

, for controlling the attitude of a vehicle comprising

means for computing a desired torque command signal to control the attitude of said vehicle and providing said torque command signal at an output terminal of said computing means,

means coupled to said output terminal of said computing means for integrating said torque command signal and producing an integrated torque command output signal,

sensing means for measuring the angular velocity, ω

, of said sensitive element and producing an output signal proportional thereto,

combining means having a first input terminal coupled to said integrating means for receiving said integrated torque command output signal and a second input terminal coupled to said means for measuring angular velocity for producing an output error signal proportional to the difference between said integrated torque command signal and said output error signal, and

motor means coupled to said combining means for receiving said output error signal and producing a torque output which is applied to said sensitive element thereby producing a change in said angular velocity, ω

, whereby the torque applied to said sensitive element is substantially equal to said commanded torque signal and is compensated for the presence of undesired disturbance torques on said assembly and anomolies in said control circuit.

2. A control torque command circuit as recited in claim 1 in which said means for integrating includes a circuit having a time constant, T₁, and a transfer function T₁ /T₁ S+1 and

said combining means includes a matching circuit coupled between its second input and said sensing means having a transfer function T₁ S/T₁ S+1.

3. A control torque command circuit as recited in claim 2 in which said matching circuit includes a first circuit coupled to said sensing means having a time constant T₂ and a second circuit coupled between said first circuit and said second input on said combining means having a time constant T₁ wherein T₂ is very much greater than T₁ and has a negligible effect on the transfer characteristic of the matching circuit.

4. A control torque command circuit as recited in claim 1 in which said combining means includes an operational amplifier having a first non-inverting input terminal and a second inverting input terminal.

5. A control torque command circuit as recited in claim 1 in which said sensing means includes tachometer means for providing an output signal indicative of the number of revolutions of said sensitive element.

6. A control torque command circuit as recited in claim 1 in which said computing means includes means for providing said torque command signal in the form of a series of pulses,

said torque command circuit further includes storage means coupled between said computing means and said integrating means for receiving said torque command signal in the form of a series of pulses, and

said integrating means includes a series circuit in which a digital subtracter circuit has a first input terminal coupled to said output terminal of said storage means and its output terminal coupled to an input terminal on a shift register which has its output terminal coupled to said first input terminal on said combining means and to a second input terminal on said digital subtracter circuit.

7. A control torque command circuit as recited in claim 6 in which said combining means includes a digital subtractor circuit for producing an output error signal in the form of a series of pulses.

8. A control torque command circuit as recited in claim 7 in which said sensing means includes a digital tachometer means for providing a number of output pulses proportional to the number of revolutions of said sensitive element.

9. A control torque command circuit as recited in claim 8 further including a series circuit comprising a counter coupled to the output terminal of said digital tachometer means and a shift register coupled between the output terminal of said counter and said second input terminal of said combining means for providing an output signal in accordance with the angular velocity, ω

, of said sensitive element.

10. A control torque command circuit as recited in claim 7 further including a series circuit coupled between the output terminal of said combining means and said motor means for converting said output error signal in the form of a series of pulses into an analog output voltage which is applied to said motor means.

11. A control troque command circuit as recited in claim 10 in which said series circuit includes a shift register having an input terminal coupled to the output terminal of said combining means for producing a parallel binary output signal in accordance with said error signal.

12. A control torque command circuit as recited in claim 11 in which said series circuit further includes a digital-to-analog converter circuit responsive to said parallel binary output signal from said shift register for providing a variable amplitude d.c. output voltage in accordance with said error signal.

13. A control torque command circuit as recited in claim 12 in which said series circuit further includes integrating circuit means having its input terminal coupled to the output terminal of said digital-to-analog converter means for providing a variable amplitude d.c. output signal above a specified minimum amplitude, which minimum amplitude signal when coupled to said motor means will maintain said sensitive element rotating at a minimum angular velocity.

14. A control torque command circuit as recited in claim 13 in which said series circuit further includes pulse width modulator means coupled to said integrating circuit means for producing a variable pulse width output signal having pulse widths proportional to the amplitude of said variable amplitude d.c. output signal.

15. A control torque command circuit as recited in claim 14 in which said series circuit further includes power bridge means coupled between said pulse width modulator means and said motor means for providing power gain to said variable pulse width output signal.

16. A control torque command circuit as recited in claim 13 in which said series circuit further includes a linear power amplifier coupled between said integrating circuit and said motor means for providing power gain to said variable amplitude d.c. signal.