Geographically limited missile

• US 6,142,411 A
• Filed: 06/26/1997
• Issued: 11/07/2000
• Est. Priority Date: 06/26/1997
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Cobleigh, Nelson E.
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): BUCKLEY, DENISE J
• Application Number:
  US08/883,637
• Time in Patent Office: 1,230 Days
• Field of Search: 244/3.14, 244/3.11, 244/3.15, 244/3.2, 102/215, 102/206, 102/211, 102/214
• US Class Current: 244/3.14
• CPC Class Codes: F41A 17/08 for inhibiting firing in a specified direction, e.g. at a friendly person or at a protected area F41A27/02 takes precedence
• CPC Class Codes: F41G 7/34 based on predetermined target position data
• CPC Class Codes: F42C 15/40 wherein the safety or arming action is effected electrically
• CPC Class Codes: F42C 9/16 for self-destruction of ammunition F42C9/141 - F42C9/148 take precedence

Abstract

A self destruct mechanism for an airborne projectile is provided. The projectile includes a navigation system which provides an absolute global position of the projectile. The position is compared with positions stored in memory. If the position of the projectile is determined to be acceptable, operation of the projectile continues. If the position of the projectile is unacceptable, an electronic control system initiates a self-destruct signal for the projectile.

Claims

1. An airborne projectile apparatus, comprising:

a navigational system which determines a position of the projectile, the navigation system providing at least one of latitude coordinate information and longitude coordinate information;

memory for storing a plurality of positions, some of the plurality of positions designated as acceptable positions for the projectile and others of the positions defined as unacceptable positions for the projectile; and

an electronic control unit which searches for a location in the memory which corresponds to the position determined by the navigation system to determine if the position of the projectile is acceptable or unacceptable, the electronic control unit initiating a self-destruct signal causing the projectile to self-destruct if the position of the projectile is unacceptable.

2. The apparatus of claim 1 wherein the navigation system includes a Global Positioning System (GPS) receiver.

3. The apparatus of claim 1 wherein the navigation system additionally provides altitude information of the projectile.

4. The apparatus of claim 3 wherein the navigation system provides at least one of speed and direction information of the projectile.

5. The apparatus of claim 1 wherein the navigation system provides the position of the projectile, based on electromagnetic signals received from an electromagnetic transmitter.

6. The apparatus of claim 1 wherein the navigational system includes an inertial navigation system.

7. The apparatus of claim 1 wherein the positions stored in memory include at least one of latitude coordinate information, longitude coordinate information, and altitude information.

8. A self-destruct apparatus for an airborne projectile comprising:

a navigational system which determines a position of the projectile in accordance with both latitude coordinate information and longitude coordinate information;

memory for storing a plurality of positions, some of the plurality of positions designated as acceptable positions for the projectile and others of the positions defined as unacceptable positions for the projectile; and

an electronic control unit which searches for a location in the memory which corresponds to the position determined by the navigation system to determine if the position of the projectile is acceptable or unacceptable, the electronic control unit initiating a self-destruct signal causing the projectile to self-destruct if the position of the projectile is unacceptable.

9. The apparatus of claim 8 wherein the navigation system includes a Global Positioning System (GPS) receiver.

10. The apparatus of claim 8 wherein the navigation system provides the position of the projectile, based on electromagnetic signals received from an electromagnetic transmitter.

11. The apparatus of claim 8 wherein the positions stored in memory include at least one of latitude coordinate information, longitude coordinate information, and altitude information.

12. The apparatus of claim 8 wherein the navigation system additionally provides altitude information of the projectile.

13. The apparatus of claim 12 wherein the navigation system provides at least one of speed and direction information of the projectile.

14. An airborne projectile apparatus, comprising:

a navigational system which determines a position of the projectile, the navigation system providing at least one of latitude coordinate information and longitude coordinate information;

memory for storing a plurality of positions; and

an electronic control unit which searches for a location in the memory which corresponds to the position determined by the navigation system to determine if the position of the projectile is acceptable or unacceptable, the electronic control unit initiating a self-destruct signal causing the projectile to self-destruct if the position of the projectile is unacceptable.