Self guided recoverable airborne instrument module

• US 5,186,418 A
• Filed: 07/31/1991
• Issued: 02/16/1993
• Est. Priority Date: 07/31/1991
• Status: Expired due to Term

• Current Assignee: University Corporation For Atmospheric Research
• Original Assignee: University Corporation For Atmospheric Research
• Inventors: Lauritsen, Dean K.
• Primary Examiner(s): Peters, Jr., Joseph F.
• Assistant Examiner(s): Ansley, VirnaLissi
• Application Number:
  US07/738,350
• Time in Patent Office: 566 Days
• Field of Search: 244/138 R, 244/138 A, 244/152, 244/32, 102/384, 102/385, 102/387, 102/348, 102/354, 342/64, 367/4
• US Class Current: 244/138.00A
• CPC Class Codes: B64D 1/00 Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight with respect to weapon sights devices F41G takes precedence, parachutes per se B64D17/00; ejectable seats B64D25/10; ejectable capsules B64D25/12; refuelling during flight B64D39/00; launching apparatus for projecting projectiles or missiles F41F1/00, F41F7/00; rocket or torpedo launchers F41F3/00
• CPC Class Codes: G01W 1/08 Adaptations of balloons, missiles, or aircraft for meteorological purposes; Radiosondes transmission of measurements G01D; transmitting circuits H04B; balloons in general B64B; aeroplanes in general B64D; missiles in general F42B15/00

Abstract

The recoverable airborne instrument module is implemented using an aerodynamic housing which has at least one moveable control surface thereon. In operation, the recoverable instrument module is carried aloft by balloon to enable its instrument package payload to perform a series of meteorological measurements. The exterior housing of the recoverable instrument package has an aerodynamic shape, such as a delta wing airframe with a controllable rudder. A navigation circuit contained within the housing references the radio frequency transmissions of a plurality of beacons to determine the altitude and geographic position of the instrument package. This information, as well as data identifying the location of at least one predetermined landing site is used to dynamically calculate a flight path to controllably descend the instrument module to a selected one of these landing sites. The guidance control circuit uses the rudder to steer the recoverable instrument module in a glide along the computed flight path to perform a controlled descent to the selected predetermined landing site. A radio frequency transmitter broadcasts present position information to act as a beacon to expedite recovery of the instrument module.

Claims

1. An unpropelled airborne module that returns to one of a plurality of ground level landing sites by gliding in a self-guided manner comprising:

an aerodynamically shaped winged exterior housing including;

at least one moveable control surface to steer said airborne module;

means for determining a geographic position of said airborne module;

means for storing, for the duration of said gliding, programmed data indicative of the geographic position of at least one of said plurality of ground level landing sites;

means, responsive to said storing of said programmed data and said determining of said geographic position of said airborne module, for computing a flight path for said airborne module to said at least one of said plurality of ground level landing sites in response to said determining of said geographic position of said airborne module; and

means, responsive to said computing of said flight path, for operating said moveable control surface to guide said airborne module along said flight path.

2. The airborne module of claim 1 further comprising:

means for measuring altitude of said airborne module; and

wherein said computing means is additionally responsive to said measured altitude to compute said flight path.

3. The airborne module of claim 1 further comprising:

means for broadcasting data, via wireless communication, indicative of said determined geographic position of said airborne module.

4. The airborne module of claim 3 further comprising:

means for periodically activating said broadcasting means when said airborne module has reached said landing site.

5. The airborne module of claim 1 further comprising:

a parachute, deployable to slow the descent of said airborne module to said landing site.

6. The airborne module of claim 5 further comprising:

means for measuring altitude of said airborne module; and

means for deploying said parachute when said measured altitude is less than a predetermined value.

7. The airborne module of claim 1 wherein said exterior housing is a delta-wing shape having a moveable control surface comprising a rudder.

8. The airborne module of claim 1 wherein said determining means includes:

means for monitoring a plurality of beacon signals generated external to said airborne module and broadcast to said airborne module; and

means, responsive to said monitored beacon signals, for computing data indicative of the geographic position of said airborne module.

9. The airborne module of claim 8 wherein said beacon signals comprise signals broadcast from a plurality of satellites.

10. The airborne module of claim 8 wherein said computing means dynamically computes said flight path on a continuing basis in response to said geographic position of said airborne module determined by said determining means, based on said monitored beacon signals.

11. The airborne module of claim 1 wherein said computing means dynamically computes said flight path on a continuing basis in response to said geographic position of said airborne module determined by said determining means.

12. A method of guiding an unpropelled airborne module that returns to one of a plurality of ground level landing sites by gliding in a self-guided manner, wherein said airborne module includes an aerodynamically shaped winged exterior housing and has at least one moveable control surface to steer said airborne module comprising the steps of:

determining a geographic position of said airborne module;

storing, for the duration of said gliding, programmed data indicative of the geographic position of said plurality of ground level landing sites;

retrieving, in response to said determining of said geographic position of said airborne module, a portion of said stored data indicative of the geographic position of one of said plurality of ground level landing sites;

computing, in response to said retrieving of said programmed data and said determining of said geographic position of said airborne module, a flight path for said airborne module to said one of said plurality of ground level landing sites; and

operating, based on said computed flight path, said moveable control surface to guide said airborne module along said flight path.

13. The method of claim 12 further comprising the step of:

measuring altitude of said airborne module to compute said flight path.

14. The method of claim 12 further comprising the step of:

broadcasting data, via wireless communication, indicative of said determined geographic position of said airborne module.

15. The method of claim 14 further comprising the step of:

periodically activating said step of broadcasting once said airborne module reaches said landing site.

16. The method of claim 12 wherein said airborne module includes a parachute, deployable to slow the descent of said airborne module to said landing site, further comprising the steps of:

measuring altitude of said airborne module; and

deploying said parachute when said measured altitude is less than a predetermined value.

17. The method of claim 12 wherein said step of determining includes:

monitoring a plurality of beacon signals generated external to said airborne module and broadcast to said airborne module; and

computing, in response to said monitored beacon signals, data indicative of the geographic position of said airborne module.

18. An unpropelled airborne module that returns to one of a plurality of predetermined ground level landing sites by gliding in a self-guided manner comprising:

an aerodynamically shaped exterior housing including;

at least one moveable control surface to steer said airborne module;

means for determining a geographic position of said airborne module, including;

means for monitoring a plurality of beacon signals generated external to said airborne module and broadcast to said airborne module,

means, responsive to said monitoring of said beacon signals, for computing data indicative of said geographic position of said airborne module;

means for storing, for the duration of said gliding, preprogrammed data indicative of the geographic position of said plurality of predetermined ground level landing sites;

means, responsive to said storing of said data and said determining of said geographic position of said airborne module, for selecting one of said plurality of said predetermined ground level landing sites as a destination landing site;

means for computing a flight path for said airborne module from said geographic position determined by said determining means to said destination landing site; and

means, responsive to said computing of said flight path, for operating said moveable control surface to guide said airborne module along said flight path.

19. The airborne module of claim 18 further comprising:

means for measuring altitude of said airborne module; and

wherein said computing means is additionally responsive to said measured altitude to compute said flight path.

20. The airborne module of claim 18 further comprising:

means for broadcasting data, via wireless communication, indicative of said determined geographic position of said airborne module.

21. The airborne module of claim 20 further comprising:

means for periodically activating said broadcasting means when said airborne module has reached said destination landing site.

22. The airborne module of claim 18 further comprising:

a parachute, deployable to slow the descent of said airborne module to said destination landing site.

23. The airborne module of claim 22 further comprising:

means for measuring altitude of said airborne module; and

means for deploying said parachute when said measured altitude is less than a predetermined value.

24. The airborne module of claim 18 wherein said exterior housing is a delta-wing shaped having a moveable control surface comprising a rudder.

25. The airborne module of claim 24 wherein said beacon signals comprise signals broadcast from a plurality of satellites.

26. The airborne module of claim 24 wherein said computing means dynamically computes said flight path on a continuing basis in response to said geographic position of said airborne module determined by said determining means, based on said monitored beacon signals.

27. The airborne module of claim 18 wherein said computing means dynamically computes said flight path on a continuing basis in response to said geographic position of said airborne module determined by said determining means.

28. A method of guiding an unpropelled airborne module that returns to one of a plurality of ground level landing sites by gliding in a self-guided manner, wherein said airborne module includes an aerodynamically shaped winged exterior housing that has at least one moveable control surface to steer said airborne module comprising the steps of:

determining a geographic position of said airborne module, including;

a monitoring a plurality of beacon signals generated external to said airborne module and broadcast to said airborne module,

computing, in response to said monitoring of said beacon signals, data indicative of the geographic position of said airborne module;

storing, for the duration of said gliding, preprogrammed data indicative of the geographic position of said plurality of ground level landing sites;

retrieving, in response to said computing of said data indicative of a determined said geographic position of said airborne module, a portion of said stored data indicative of the geographic position of a selected one of said plurality of ground level landing sites;

computing, in response to said retrieving of said data indicative of said geographic position of said selected one of said plurality of ground level landing sites and said determined geographic position of said airborne module, a flight path for said airborne module from said determined geographic position of said airborne module to said selected one of said plurality of said landing sites; and

operating, based on said computed flight path, said moveable control surface to guide said airborne module along said flight path.

29. The method of claim 28 further comprising the step of:

measuring altitude of said airborne module to compute said flight path.

30. The method of claim 28 further comprising the step of:

broadcasting data, via wireless communication, indicative of said determined geographic position of said airborne module.

31. The method of claim 30 further comprising the step of:

periodically activating said step of broadcasting once said airborne module reaches said landing site.

32. The method of claim 28 wherein said airborne module includes a parachute, deployable to slow the descent of said airborne module to said landing site, further comprising the steps of:

measuring altitude of said airborne module; and

deploying said parachute when said measured altitude is less than a predetermined value.