Simulator of mechanical properties of a steering system

• US 4,708,656 A
• Filed: 02/04/1986
• Issued: 11/24/1987
• Est. Priority Date: 11/11/1985
• Status: Expired due to Fees

• Current Assignee: Fokker (CDR) BV (Melrose Industries Plc)
• Original Assignee: Fokker (CDR) BV (Melrose Industries Plc)
• Inventors: Wierda, Gerhard J., de Vries, Luitzen
• Primary Examiner(s): Picard, Leo P.
• Application Number:
  US06/826,029
• Time in Patent Office: 658 Days
• Field of Search: 434/45, 434/29
• US Class Current: 434/45
• CPC Class Codes: G09B 9/28 Simulation of stick forces or the like

Abstract

A simulator of previously chosen mechanical properties of the steering system of a device such as an aircraft employs a controllable limiter for simulating the mechanical Coulomb friction of the control member and is arranged in a negative feedback loop and having two control signal inputs which determine the maximum and minimum outputs of the limiter in association with a further input signal corresponding to the friction concerning the control member. The limiter interrupts output until the level of the Coulomb friction to be simulated is exceeded.

Claims

1. In a flight simulator or similar system which includes a manually operated control member and a servo means connected thereto for acting and reacting on the control member to simulate response of a controlled member such as a control surface under flight conditions, said servo means including a servo valve, amplifier means for controlling the servo valve in response to a plurality of inputs thereto, computer means for producing flight simulating signals, electrical analogue means by producing output signals feeding the amplifier means and including a combining circuit, a divider and first and second integrators, all in series, the combining circuit having an input from the computer means which represents simulated flight conditions, pick-up means having an output which represents manual input force applied to the control member, a second amplifier having the output of the pick-up means connected as an input thereto and the output of the second integrator as an input thereto and having an output representing position error of the control member which is connected to the amplifier means, the divider dividing the output of the combining circuit by a value representing the mass of the control member to produce a control member acceleration-related signal applied to the first integrator whereby the output of the first integrator is a control member velocity-related signal and the output of the second integrator is a control member position-related signal, the acceleration-related signal and the velocity-related signal being connected as inputs to the amplifier means, the improvement comprising controllable limiter means connected in negative feedback relation from the output of the first integrator to the input to the divider for simulating the mechanical Coulomb friction of the control member, and control means connected between the combining circuit and the limiter for providing sum and difference signals, respectively, of the output of the combining circuit and an external friction signal to the limiter.

2. In a flight simulator as defined in claim 1 wherein the limiter includes an amplifier.

3. In a flight simulator as defined in claim 2 wherein the limiter includes two diode circuits in series and reverse biased by the sum and difference signals, the junction between the diodes of the diode circuits being connected to the input of the divider and coupled with the output of the first integrator.

4. In a flight simulator as defined in claim 3 wherein each diode circuit includes an operational amplifier, each having an input connected to the junction with one of the operational amplifiers having another input connected to the sum signal and the other of the operational amplifiers having another input connected to the difference signal.

5. In a flight simulator as defined in claim 4 wherein the computer means is of the digital type, an analogue/digital converter connecting the output of the first integrator with the computer means, and a digital/analogue converter connecting the computer means to the combining circuit.

6. In a flight simulator as defined in claim 5 wherein the second integrator is of the digital type connected to the output of the analogue/digital converter, and including a second digital/analogue converter connecting the output of the second integrator to the second amplifier.

7. In a flight simulator as defined in claim 6 including a summing circuit having the output of the first integrator as one input and the inverted output of the second integrator as a second input and coupled with the junction, and a further summing circuit for addition to the inverted output of the second integrator.

8. In a flight simulator as defined in claim 1 wherein the limiter includes two diode circuits in series and reverse biased by the sum and difference signals, the junction between the diodes of the diode circuits being connected to the input of the divider and coupled with the output of the first integrator.

9. In a flight simulator as defined in claim 8 wherein each diode circuit includes an operational amplifier, each having an input connected to the junction with one of the operational amplifiers having another input connected to the sum signal and the other of the operational amplifiers having another input connected to the difference signal.

10. In a flight simulator as defined in claim 1 wherein the computer means is of the digital type, an analogue/digital converter connecting the output of the first integrator with the computer means, and a digital/analogue converter connecting the computer means to the combining circuit.

11. In a flight simulator as defined in claim 10 wherein the second integrator is of the digital type connected to the output of the analogue/digital converter, and including a second digital/analogue converter connecting the output of the second integrator to the second amplifier.

12. In a flight simulator as defined in claim 11 including a summing circuit having the output of the first integrator as one input and the inverted output of the second integrator as a second input and coupled with the junction, and a further summing circuit for addition to the inverted output of the second integrator.

13. A flight simulator comprising a flight-simulation computer, at least one control element, servo-means coupled with the or each element and including an amplifier, said computer being coupled with the amplifier through an electric analog representing the relevant mechanical properties of the element concerned, the electric analog comprising a divider for dividing its input signal by a value proportional to the desired mass of the element, the output of the divider being coupled with as third input of the amplifier, a first integrator connected to the output of the divider, and a second integrator connected to the output of the first integrator, the output of the second integrator being coupled with the input of the amplifier, the improvement comprising controllable limiter means connected in negative feedback relation from the output of the first integrator to the input to the divider for simulating the mechanical Coulomb friction of the control member, and control means connected between the amplifier and the limiter for providing sum and difference signals, respectively, of the output of the amplifier and an external friction signal to the limiter.

14. A flight simulator as defined in claim 13 wherein the limiter includes two diode circuits in series and reverse biased by the sum and difference signals, the junction between the diodes of the diode circuits being connected to the input of the divider and coupled with the output of the first integrator.

15. In a flight simulator as defined in claim 14 wherein each diode circuit includes an operational amplifier, each having an input connected to the junction with one of the operational amplifiers having another input connected to the sum signal and the other of the operational amplifiers having another input connected to the difference signal.

16. A flight simulator as defined in claim 15 wherein the computer is of the digital type, an analogue/digital converter connecting the output of the first integrator with the computer, and a digital/analogue converter connecting the computer to the amplifier.

17. A flight simulator as defined in claim 16 wherein the second integrator is of the digital type connected to the output of the analogue/digital converter, and including a second digital/analogue converter connected to the output of the second integrator.

18. A flight simulator as defined in claim 17 including a summing circuit having the output of the first integrator as one input and the inverted output of the second integrator as a second input and coupled with the junction, and a further summing circuit for addition to the inverted output of the second integrator.

19. A flight simulator as defined in claim 13 wherein the computer is of the digital type, an analogue/digital converter connecting the output of the first integrator with the computer, and a digital/analogue converter connecting the computer to the amplifier.

20. A flight simulator as defined in claim 19 wherein the second integrator is of the digital type connected to the output of the analogue/digital converter, and including a second digital/analogue converter connecting the output of the second integrator to the second amplifier.