Optical position and orientation measurement techniques

• US 4,649,504 A
• Filed: 05/22/1984
• Issued: 03/10/1987
• Est. Priority Date: 05/22/1984
• Status: Expired due to Fees

• Current Assignee: CAE USA Incorporated (CAE Incorporated)
• Original Assignee: CAE USA Incorporated (CAE Incorporated)
• Inventors: Krouglicof, Nicholas, Svoboda, Jaroslav, McKinnon, Gordon M.
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Dixon, Joseph L.
• Application Number:
  US06/613,063
• Time in Patent Office: 1,022 Days
• Field of Search: 364/559, 364/578, 340/705, 340/712, 340/709, 340/825.19, 340/980, 356/141, 356/152
• US Class Current: 702/153
• CPC Class Codes: G01S 5/163 Determination of attitude using inertial means G01C9/00; control of attitude G05D1/49

Abstract

A non-contact sensing system for monitoring the position and orientation of a rigid body in space having at least three distinct point light sources mounted on the rigid body. At least two position sensor heads are fixedly mounted within detection range of light from the light sources, each position sensor head having a position sensitive detector. The lights are illuminated one at a time and in sequential arrangement and a processor computes the position in three-dimensional space of an illuminated light source with data provided simultaneously by both position sensitive detectors. The processor means also computes the position of the object in all six degrees of freedom using the three-dimensional positional data of all three light sources.

Claims

1. A non-contact sensing system for monitoring the position and orientation of a rigid body in space wherein at least three distinct point light sources are mounted on said body for movement therewith;

said system comprising;

at least two position sensor heads fixedly mounted within detection range of light from all of said light sources, said position sensor heads being directed at said light sources;

wherein each position sensor head includes a position sensitive detector;

means for turning said light sources on one at a time and in a sequential arrangement;

processor means;

said position sensitive detector outputs being connected to the input of said processor means;

said processor means computing the position in three-dimensional space of a turned on light source with data concerning said turned on light source provided simultaneously by both position sensitive detectors;

said processor means also computing the position of said object in all six degrees of freedom using the three-dimensional positional data of all three light sources;

said processor means further selecting which light source is to be turned on and driving said means for turning said light source on, whereby said computer has data concerning which light source is turned on at any time.

2. A system as defined in claim 1 wherein said position sensitive detectors provide analog signals at their outputs;

analog-to-digital conversion means between the outputs of said position sensitive detectors and the input of said processing means whereby to convert said analog signals into digital signals for use in said processor means.

3. A system as defined in claim 2 and including means for varying power to said light sources whereby to maintain a constant light intensity from each light source, when the light source is turned on, at said position sensitive detectors regardless of the position and orientation of said rigid body.

4. A system as defined in claim 3 and further including lens means on each position sensor head whereby to focus light from said light sources onto a respective position sensitive detector.

5. A system as defined in claim 4 and including filter means on each lens, the filter means being spectrally matched to the light sources.

6. A system as defined in claim 5 wherein said rigid body comprises a pilot'"'"'s helmet within the cockpit of an aircraft simulator;

said position sensor heads being mounted in the interior of said simulator.

7. A system as defined in claim 6 wherein said light sources comprise LEDs, said means for varying the power to said light sources comprising means for varying the current to said LEDs.

8. A non-contact method for monitoring the position and orientation of a rigid body in space having at least three distinct point light sources mounted thereon for movement therewith;

at least two position sensor heads fixedly mounted within detection range of light from said light sources, each position sensor head including a position sensitive detector, said position sensor heads being directed at said light sources;

and a processor means;

said method comprising;

turning on said light sources one at a time and in sequential arrangement;

computing, by said processor means, the position in three-dimensional space of a turned on light source with data concerning said turned on light source provided simultaneously by both position sensitive detectors to said processor means;

computing the position of said object in all six degrees of freedom using the three-dimensional positional data of all three light sources.