The present invention is directed to missile training systems, especially to those relating to the provision of a mechanism that allows missiles and similar devices to be fired at a target in a realistic, but safe, manner. The use of live fire exercises, in which army or other armed forces personnel
The present invention is directed to missile training systems, especially to those relating to the provision of a mechanism that allows missiles and similar devices to be fired at a target in a realistic, but safe, manner. The use of live fire exercises, in which army or other armed forces personnel use fully functioning weapons systems is well established. Live fire exercises can be used to provide realistic training scenarios, but also present obvious dangers. The present invention provides a module for attachment to an object (such as a missile), the object being adapted to be directed towards a target (such as a ship), the module comprising a control system providing an output signal indicative of whether or not said object is to be destroyed.
대표청구항▼
1. A generic module for external attachment to a missile, torpedo or other projectile, the missile, torpedo or other projectile being configured for directing towards a target in testing of missile defence systems or live fire exercises, the module comprising: a position detector for providing posit
1. A generic module for external attachment to a missile, torpedo or other projectile, the missile, torpedo or other projectile being configured for directing towards a target in testing of missile defence systems or live fire exercises, the module comprising: a position detector for providing position data;a mechanism for destroying said missile, torpedo or other projectile; anda control system configured to receive said position data from the position detector and to provide an output signal to the mechanism for destroying the missile, torpedo or other projectile to cause said mechanism to destroy the missile, torpedo or other projectile if the position detector indicates that said missile, torpedo or other projectile is in an unsafe position. 2. A module as claimed in claim 1, wherein the control system is configured to provide the output signal if the missile, torpedo or other projectile is not positioned within an allowed zone, the zone being defined according to an anticipated path of the missile, torpedo or other projectile. 3. A module as claimed in claim 1, wherein said position detector comprises two or more independent position detector systems. 4. A module as claimed in claim 3, further comprising means for providing a single position signal in response to data from the said two or more independent position detector systems. 5. A module as claimed in claim 4, wherein the control system is arranged to provide the output signal if the missile, torpedo or other projectile is not positioned within an allowed zone, the zone being defined according to an anticipated path of the missile, torpedo or other projectile. 6. A module as claimed in claim 1, further comprising a transmitter for transmitting data to a central server. 7. A module as claimed in claim 6, wherein said data includes position data. 8. A module as claimed in claim 1, further comprising means for mechanically attaching the module to said missile, torpedo or other projectile. 9. A system comprising a module as claimed in claim 1, and further comprising the missile, torpedo or other projectile, in which the module and the missile, torpedo or other projectile are connected by a connection that is solely mechanical. 10. A method comprising the steps of: directing a missile, torpedo or other projectile towards a target, the missile, torpedo or other projectile having a module externally attached thereto;determining by using a control system of the module the position of the module using position data received from a position detector of the module, the position detector comprising two or more position sensors, the control system generating and sending a signal to the module for destroying the missile, torpedo or other projectile if the missile, torpedo or other projectile is in an unsafe position. 11. A method as claimed in claim 10, further comprising the steps of defining allowed and disallowed zones for said missile, torpedo or other projectile, wherein the signal for destroying the missile, torpedo or other projectile is activated if the missile, torpedo or other projectile is within a disallowed zone. 12. A method as claimed in claim 10, wherein the step of determining the position of the module includes the step of using two or more independent position detector systems. 13. A method as claimed in claim 12, wherein the step of using said module to destroy the missile, torpedo or other projectile is carried out if any of said position detector systems indicate that the missile, torpedo or other projectile is in a disallowed zone. 14. A method as claimed in claim 12, wherein the step of determining the position of the module comprises outputting a single position signal in response to data from the said two or more independent position detector systems. 15. A method as claimed in claim 10, further comprising the step of transmitting data to a central server. 16. A method as claimed in claim 15, wherein said data includes position data. 17. A method as claimed in claim 10, further comprising the step of mechanically attaching the module to said missile, torpedo or other projectile. 18. A method comprising the steps of: directing a missile, torpedo or other projectile at a target;determining the position of the missile, torpedo or other projectile using a position detector;transmitting data concerning the position of the missile, torpedo or other projectile to a remote server; anddestroying the missing, torpedo or other projectile if one of a number of conditions is not met. 19. A method as claimed in claim 18, further comprising the step of attaching a module to the missile, torpedo or other projectile. 20. A method as claimed in claim 19, further comprising the step of using said module to obtain the said position of the missile, torpedo or other projectile. 21. A method as claimed in claim 19, wherein the step of destroying the missile, torpedo or other projectile is carried out by use of the module to destroy the missile, torpedo or other projectile. 22. A method as claimed in claim 18, further comprising the step of defining allowed and disallowed zones for said missile, torpedo or other projectile, wherein the step of destroying the missile, torpedo or other projectile is activated if the missile, torpedo or other projectile is within a disallowed zone. 23. A method as claimed in claim 18, wherein the step of the determining the position of the missile includes the step of using two or more independent position detector systems.
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이 특허에 인용된 특허 (23)
Linick James M. (P.O. Box 1512 La Quinta CA 92253), Apparatus and method for remote guidance of cannon-launched projectiles.
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