Parafoil electronic control unit having wireless connectivity

• US 8,818,581 B2
• Filed: 04/08/2011
• Issued: 08/26/2014
• Est. Priority Date: 04/13/2010
• Status: Active Grant

• Current Assignee: The Government Of The United States Of America, As Represented By The Secretary Of The Navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Bourakov, Eugene, Yakimenko, Oleg
• Primary Examiner(s): Black, Thomas G
• Assistant Examiner(s): NELSON, SARA J
• Application Number:
  US13/083,506
• Publication Number:
  US 20130009013A1
• Time in Patent Office: 1,236 Days
• Field of Search: 379/88.04, 701 3- 18, 244/76.R, 244/175, 244/189
• US Class Current: 701/16
• CPC Class Codes: B64D 1/08 the articles being load-carrying devices
• CPC Class Codes: B64D 17/00 Parachutes non canopied parachutes B64D19/00
• CPC Class Codes: B64D 17/025 for gliding chutes
• CPC Class Codes: G05D 1/0684 on a moving platform, e.g. aircraft carrier
• CPC Class Codes: G05D 1/105 specially adapted for unpowered flight, e.g. glider, parachuting, forced landing parachutes per se B64D17/00
• CPC Class Codes: H04B 7/18504 Aircraft used as relay or high altitude atmospheric platform
• CPC Class Codes: H04W 48/16 Discovering, processing access restriction or access information

Abstract

A method is described that includes performing a), b) and c) below with an electronic control unit of a parafoil: a) after being dropped from an airborne vehicle, wirelessly receiving the parafoil'"'"'s desired landing location; b) determining a flight path for the parafoil that lands at the desired landing location; and, c) controlling the parafoil'"'"'s flight path consistently with the determined flight path.

Claims

1. A method, comprising:

performing a), b), c) and d) below with an electronic control unit of a parafoil;

a) after being dropped from an airborne vehicle, receiving through a wireless network interface circuitry a desired landing location for said parafoil, barometric pressure at said desired landing location, and a most current wind versus altitude profile, said most current wind versus altitude profile including a magnitude and direction of ground winds and winds at higher altitudes;

b) determining a determined flight path for said parafoil that lands said parafoil at said desired landing location;

c) controlling said parafoil to travel on a flight path consistent with said determined flight path; and

,

d) wirelessly receiving one or more updates, each of said updates including an updated ground barometric pressure and an updated wind versus altitude profile, and repeating b) and c) based on each of said one or more updates;

wherein said desired landing location and said one or more updates are wirelessly transmitted into a wireless network by electronic equipment, and, said desired landing location, said barometric pressure at said desired landing location, said most current wind versus altitude profile, and said one or more updates are wirelessly received at said electronic control unit from said wireless network over a wireless link established between said electronic equipment and said electronic control unit.

2. The method of claim 1 wherein said wireless network is a GSM network.

3. The method of claim 1 further comprising entering said desired landing location into said electronic equipment.

4. The method of claim 3 wherein said desired landing location is entered into said electronic equipment verbally by way of a verbal command.

5. The method of claim 4 further comprising sending said verbal command over a network to a voice recognition engine, converting said verbal command into an electronic format and sending said desired landing location over said network as a command to said electronic control unit.

6. An apparatus, comprising:

an electronic control unit for a parafoil comprising;

a) wireless receiver circuitry comprising;

means for receiving through a wireless network interface circuitry a desired landing location for said parafoil, barometric pressure at said desired landing location, and a most current wind versus altitude profile, said most current wind versus altitude profile including a magnitude and direction of ground winds and winds at higher altitudes, and

means for wirelessly receiving one or more updates including an updated ground barometric pressure and an updated wind versus altitude profile;

b) means for adjusting trailing edge lines of said parafoil; and

c) a storage medium and a processing core, said storage medium containing program code that when processed by said processing core causes said control unit to perform the following method;

determining a determined flight path for said parafoil that lands said parafoil at said desired landing location;

updating said determined flight path based on said one or more updates; and

,

controlling said parafoil to travel on a flight path consistent with said determined flight path.

7. The apparatus of claim 6 wherein said wireless receiver circuitry comprises means to establish a wireless link with electronic equipment that transmits a desired landing location for said parafoil, barometric pressure at said desired landing location, and a most current wind versus altitude profile, said most current wind versus altitude profile including a magnitude and direction of ground winds and winds at higher altitudes.

8. The apparatus of claim 6 wherein said electronic control unit further comprises a plurality of sensors, said sensors comprising means to measure a position of said parafoil and an orientation of said parafoil.

9. The apparatus of claim 6 wherein said electronic control unit further comprises electronic transmission circuitry to wirelessly transmit at least one of a position of said parafoil, an orientation of said parafoil, and one or more loitering parameters.

10. The apparatus of claim 6 wherein said wireless receiver circuitry is compatible with a wireless network.

11. The apparatus of claim 6 wherein said wireless network is a GSM network.

12. A method, comprising:

wirelessly receiving over a wireless network position information from each of a plurality of simultaneously descending parafoils, each said position information indicating a respective position of each of said parafoils in the midst of their respective descent, said position information each being wirelessly transmitted from said parafoils over said wireless network;

determining separate desired landing locations for each one of said parafoils;

wirelessly transmitting over said wireless network to each one of said parafoils a respective desired landing location of said separate desired landing locations, each respective desired landing location to be wirelessly received over said wireless network by a respective descending parafoil;

receiving through a wireless network interface circuitry a barometric pressure at said desired landing location, and a most current wind versus altitude profile, said most current wind versus altitude profile including a magnitude and direction of ground winds and winds at higher altitudes from one or more of said parafoils;

redetermining said separate desired landing locations for one or more of said parafoils based on said barometric pressure at said desired landing location, and a most current wind versus altitude profile; and

wirelessly transmitting over said wireless network to one or more of said parafoils a redetermined respective desired landing location, each respective redetermined respective desired landing location to be wirelessly received over said wireless network by a respective descending parafoil.

13. The method of claim 12 wherein said method is performed on a computing system coupled to said wireless network.

14. The method of claim 13 wherein said wireless network is a GSM network.