Automatic guidance unit for aerial delivery unit

• US 6,587,762 B1
• Filed: 08/10/2001
• Issued: 07/01/2003
• Est. Priority Date: 08/18/2000
• Status: Expired due to Fees

• Current Assignee: FXC Corporation
• Original Assignee: FXC Corporation
• Inventors: Rooney, Harry B.
• Primary Examiner(s): Black, Thomas G.
• Assistant Examiner(s): MANCHO, RONNIE M
• Application Number:
  US09/928,222
• Time in Patent Office: 690 Days
• Field of Search: 701/3, 701/4, 701/11, 701/16, 701/201, 701/202, 701/207, 701/213, 701/217, 701/220, 235/375, 342/386, 342/357.08, 342/465, 342/357.06, 244/139, 244/3.1, 244/13, 244/164, 244/171, 244/35.R, 244/76.R, 244/152, 710/100, 710/21-23, 379/93.06, 379/357, 340/5.65, 340/996, 361/807, 361/809, 73/2, 732/00
• US Class Current: 701/16
• CPC Class Codes: B64D 1/08 the articles being load-carrying devices
• CPC Class Codes: B64D 17/34 adapted to control direction or rate of descent
• CPC Class Codes: G05D 1/105 specially adapted for unpowered flight, e.g. glider, parachuting, forced landing parachutes per se B64D17/00

Abstract

Methods and systems for programming the automatic guidance unit of an aerial delivery system. The operator selects on a hand-held unit the desired flight parameters such as the latitude, longitude and altitude of the desired landing site, as well as the desired landing heading and default heading. A microprocessor converts this data into digital data that is stored on a removable EEPROM memory key. This key is then removed from the hand-held unit and at any convenient time, inserted into a mating female receptacle in the automatic guidance unit of the aerial delivery system. The programmed information originally entered in the hand-held unit is then transferred into the guidance unit of the aerial delivery system.

Claims

1. The method of preprogramming the flight computer of a guidance unit in an automatically controlled ram air parafoil aerial delivery system comprising:

storing the latitude, longitude, altitude, desired landing heading, and default landing heading of the targeted location of said aerial delivery system as digital data in the digital memory of a microprocessor located in a handheld unit;

transferring the digital data stored in said digital memory to a removable key having a data memory integral therewith; and

removing said key from said handheld unit and inserting said key into a mating receptacle of said guidance unit to transfer data stored from said memory key into said flight computer.

2. The method of preprogramming the flight computer of an automatically controlled ram air parafoil aerial delivery system comprising:

storing the geographical coordinates of the targeted location of said aerial delivery system as digital data in the digital memory of a microprocessor located in a handheld unit;

loading data corresponding to said stored digital data in a removable device having a data memory integral therewith; and

removing said removable device from said handheld unit and inserting said device into a mating receptacle of said guidance unit to transfer data stored from said removable device into said flight computer.

3. The method of preprogramming a flight computer for a guidance unit of an aerial delivery system comprising:

entering the location of the landing target of said aerial delivery system into a memory key at a location removed from said flight computer;

moving said memory key from said remote location to said flight computer; and

using said memory key to preprogram said flight computer.

4. The method of claim 3, including causing a visible lamp to blink when said flight computer has been preprogrammed.

5. A system for preprogramming a flight computer for an automatically controlled ram air parafoil aerial delivery system comprising:

a handheld unit having a series of thumbwheel switches on which can be manually entered the latitude, longitude, altitude, desired landing heading, and default landing heading;

a microprocessor and associated computer memory within said handheld unit storing digital data which corresponds with the values manually entered using said thumbwheel switches;

a female memory key receptacle accessible on the outside of said handheld unit, such receptacle connected to said microprocessor and associated computer memory;

a memory key having an integral data memory insertable into said receptacle and storing in said integral memory data corresponding to said values manually entered using said thumbwheel switches; and

a second female receptacle mating with said memory key, said second receptacle connected to the said flight computer.

6. A system for preprogramming a flight computer for an automatically controlled ram air parafoil aerial delivery system comprising:

a handheld unit having a series of thumbwheel switches on which can be manually entered the latitude, longitude, altitude, barometric pressure, and desired landing heading;

a microprocessor and associated computer memory within said handheld unit storing digital data which corresponds with the values manually entered using said thumbwheel switches;

a female memory key receptacle accessible on the outside of said handheld unit, such receptacle connected to said microprocessor and associated computer memory;

a memory key having an integral data memory insertable into said receptacle and storing in said integral memory data corresponding to said values manually entered using said thumbwheel switches; and

a second female receptacle mating with said memory key, said second receptacle connected to the said flight computer.

7. A system for preprogramming a flight computer for an automatically controlled aerial delivery system comprising:

a unit within which the location and other parameters relating to a predetermined target location are manually entered, said unit including a computer memory storage of data corresponding to said manually entered parameters;

a first key receptacle coupled to said computer memory;

a data memory key insertable in said first key receptacle; and

a second key receptacle which accepts said memory key, said second receptacle coupled to said flight computer.

8. The system of claim 7 wherein manually entered parameters indicate the altitude of the targeted location landing site.

9. The system of claim 7 wherein said manually entered parameters include the desired landing heading.

10. The system of claim 7 wherein said manually entered parameters include the default landing heading.

11. The system of claim 7 wherein said manually entered parameters include the barometric pressure.

12. The method of preprogramming a flight computer comprising:

storing in a computer memory digital data corresponding to the location of the targeted location;

inserting a removable key having a memory integral therewith into a first receptacle coupled to said computer memory;

loading digital data in the memory of said removable key corresponding to said digital data stored in said computer memory;

removing said removable key;

inserting said removable key into a second receptacle coupled to said flight computer; and

transferring the digital data stored on said memory key to said flight computer.