Simulator control loading inertia compensator

• US 4,236,325 A
• Filed: 12/26/1978
• Issued: 12/02/1980
• Est. Priority Date: 12/26/1978
• Status: Expired due to Term

• Current Assignee: AAI Microflite Simulation International
• Original Assignee: Singer PLC (Hayleys Plc)
• Inventors: Hall, John D., Williams, Alfred S. Jr.
• Primary Examiner(s): Hum, Vance Y.
• Application Number:
  US05/973,428
• Time in Patent Office: 707 Days
• Field of Search: 35/12 S, 35/12 W, 35/12 K, 244/83 D
• US Class Current: 434/45
• CPC Class Codes: G09B 9/28 Simulation of stick forces or the like

Abstract

Signals are developed representative of the mechanical inertia of a vehicle simulator linkage elements that drive control members utilized by a student operator. These signals are combined with signals representative of programmed vehicle operating data and signals representative of the student operator'"'"'s mechanical input such that the mechanical inertia of the simulator linkage elements does not influence the signal which causes the actual operator control member to have an appropriate force/"feel".

Claims

1. In a simulator control loading system which includes a control member, a control member actuator, linkage elements therebetween, a force cell for providing a control force signal substantially representative of the total forces on the control member and including the mechanical inertia effects of the linkage elements, command means for providing a command signal representative of desired control member forces for realistic control member performance simulation, and summing means for summing said control force signal and said command signal to produce a difference signal representative of their difference for use in deriving a drive signal for actuating the actuator to produce said desired control member forces in said control member, an improvement for canceling the effect of the mechanical inertia of the linkage elements, comprising the following additional apparatus:

(a) sensing means connected to the linkage elements for producing a movement signal representative of their movement;

(b) conversion means responsive to said sensing means for converting said movement signal into an inertial force signal representative of the linkage element inertial force portion of the total forces on the control member;

(c) combining means for combining said inertial force signal with the control force signal such that said inertial force signal is subtracted from the control force signal from said force cell to thereby cancel the inertial effect of the linkage elements.

2. The apparatus of claim 1 wherein said movement signal is representative of position, and wherein said conversion means comprise:

(a) a first differentiation circuit responsive to said movement signal for developing a signal representative of the velocity of said linkage elements;

(b) a second differentiation circuit responsive to said signal representative of velocity, for developing a signal representative of the acceleration of said linkage elements; and

(c) means to scale said acceleration signal in proportion to the mass of said linkage elements such that said inertial force signal is developed.