Method and apparatus for utilizing a movable GPS antenna for surveying purposes

• US 5,182,566 A
• Filed: 10/02/1991
• Issued: 01/26/1993
• Est. Priority Date: 10/02/1991
• Status: Expired due to Fees

• Current Assignee: Geosurv Incorporated, Photocompilation PMS Incorporated
• Original Assignee: Geosurv Incorporated, Photocompilation PMS Incorporated
• Inventors: Ferguson, James, Pelletier, Luc
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US07/769,727
• Time in Patent Office: 482 Days
• Field of Search: 342/357, 343/705, 343/708, 343/713, 343/878, 343/892, 343/888, 343/889, 218/535, 218/538, 218/581
• US Class Current: 342/357.52
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
• CPC Class Codes: H01Q 1/1235 Collapsible supports; Means for erecting a rigid antenna
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons

Abstract

A method for obtaining Global Positioning System (GPS) information for a required point on the earth'"'"'s surface, the method comprising: positioning a GPS receiving antenna on a known point, beginning to record received GPS signals and thereafter continuously recording the signals, removably mounting the antenna on a rotary wing aircraft, moving the aircraft to a position proximate the required point, removing the antenna from the aircraft and positioning the antenna on the required point.

Claims

1. Apparatus for mounting on a rotary wing aircraft for supporting a Global Positioning Systems (GPS) receiving antenna, said apparatus comprising:

a boom structure for being fixed to and extending laterally to a side of said aircraft;

mounting means on said boom for cooperating with corresponding mounting means on said antenna for removably mounting said antenna on said boom; and

cable receiving means extending between said aircraft and said antenna and associated with said boom structure for receiving a communications cable attached to said antenna, wherein said cable receiving means permits the extension or retraction of said communications cable for allowing said antenna to be removed from said boom while maintaining operative communication of said antenna with said aircraft.

2. The apparatus of claim 1 wherein said boom structure comprises a group of elongated tubular members supported at their inner ends on said aircraft and which are interconnected at their outer ends, and a series of support cables for supporting and stabilizing said tubular members.

3. The apparatus of claim 1 wherein said mounting means on said boom comprises a vertically oriented tubular member for receiving a cooperating member on said antenna.

4. The apparatus of claim 3 wherein said vertically oriented member includes means for locking said cooperating member in position in or on said vertically oriented tubular member.

5. The apparatus of claim 4 wherein said means for locking comprises a pin for engagement in aligned openings in said vertically oriented tubular member and said cooperating member.

6. The apparatus of claim 5 wherein said pin is spring loaded.

7. The apparatus of claim 1 wherein said cable is a coaxial antenna cable.

8. The apparatus of claim 1 wherein said cable receiving means comprises an additional elongated tubular member secured to at least one of said group of tubular members, said additional member being for receiving and permitting relative longitudinal movement of said cable through the interior of said additional member.

9. The apparatus of claim 2 wherein said aircraft includes a fuselage and a pair of landing skids and wherein said group of elongated members comprises first and second members extending outwardly and upwardly from first and second points in a lower part of said fuselage, and a third member extending rearwardly from said outer ends of said tubular members to a third point on an upper part of said fuselage.

10. The apparatus of claim 9 wherein said series of support cables includes a first crossed pair of cables extending between positions intermediate inner and outer ends of said first and second members respectively to said second and first points in said fuselage;

a second pair of cables extending from said positions intermediate said ends to a point intermediate first and second ends of an adjacent said skid; and

a third pair of cables extending from said points intermediate said ends to a point on an upper part of said fuselage.

11. The apparatus of claim 10 including a triangular spreader structure comprising three tubular members extending between said positions intermediate the ends of said first and second members, and between said positions and an adjacent position on said third member.

12. The apparatus of claim 11 wherein said first, second and third members are reinforced at said positions.

13. Apparatus for mounting a Global Positioning Systems (GPS) receiving antenna on a rotary wing aircraft having a series of rotor blades mounted on a rotary wing assembly, said apparatus comprising:

a boom structure for being fixed to and extending laterally to a side of said aircraft and downwardly of said rotary wing assembly; and

mounting means on said boom structure for cooperating with corresponding mounting means on said antenna for removably mounting said antenna on said boom;

wherein said mounting means on said boom is positioned outwardly of said aircraft and below said rotor blades at a distance from said aircraft such that for a non-zero speed of rotation of said rotor the rotor blades will not interfere with the reception of signals from a GPS satellite by said antenna.

14. The apparatus of claim 13 wherein said boom structure comprises a group of elongated tubular members supported at their inner ends on said aircraft and interconnected at their outer ends and further comprises a series of support cables for supporting and stabilizing said tubular members.

15. The apparatus of claim 14 wherein said mounting means on said boom comprises a vertically oriented tubular member for receiving a cooperating member on said antenna.

16. The apparatus of claim 15 wherein said vertically oriented member includes means for locking said cooperating member in position in or on said vertically oriented tubular member.

17. The apparatus of claim 16 wherein said means for locking comprises a pin for engagement in aligned openings in said vertically oriented tubular member and said cooperating member.

18. The apparatus of claim 17 wherein said pin is spring loaded.

19. The apparatus of claim 14 wherein said boom structure comprises, in addition, means for supporting a communications cable extending between said aircraft and said antenna.

20. The apparatus of claim 19 wherein said cable is a coaxial antenna cable.

21. The apparatus of claim 19 wherein said means for carrying comprises an additional elongated tubular member for receiving said cable through the interior thereof, said additional member being secured to at least one of said group of tubular members.

22. The apparatus of claim 14 wherein said aircraft includes a fuselage and a pair of landing skids and wherein said group of elongated members comprises first and second members extending outwardly and upwardly from first and second points in a lower part of said fuselage, and a third member extending rearwardly from said outer ends of said tubular members to a third point on an upper part of said fuselage.

23. The apparatus of claim 22 wherein said series of support cables includes a first crossed pair of cables extending between positions intermediate inner and outer ends of said first and second members respectively to said second and first points on said fuselage;

a second pair of cables extending from said positions intermediate said ends to a point intermediate first and second ends of an adjacent said skid; and

a third pair of cables extending from said points intermediate said ends to a point on an upper part of said fuselage.

24. The apparatus of claim 23 including a triangular spreader structure comprising three tubular members extending between said positions intermediate the ends of said first and second members, and between said positions and an adjacent position on said third member.

25. The apparatus of claim 24 wherein said first, second and third members are reinforced at said positions.

26. Apparatus for mounting on a rotary wing aircraft for supporting a Global Positioning Systems (GPS) receiving antenna, said apparatus comprising:

a boom structure for being fixed to and extending laterally to a side of said aircraft;

mounting means on said boom for cooperating with corresponding mounting means on said antenna for removably mounting said antenna on said boom;

cable receiving means extending between said aircraft and said antenna and associated with said boom structure for receiving a communications cable attached to said antenna, wherein said cable receiving means permits the extension or retraction of said communications cable for allowing said antenna to be removed from said boom while maintaining operative communication of said antenna with said aircraft; and

wherein said mounting means on said boom is positioned outwardly of said aircraft and below said rotor blades at a distance from said aircraft such that for a non-zero speed of rotation of said rotor blades the rotor blades will not interfere with the reception of signals from a GPS satellite by said antenna.