Process for the autonomous positional control of guided missiles
First Claim
1. A process for the autonomous positional control of guided missiles, the guided missiles being launched from a carrier airplane, without cooperation from the carrier airplane, the process comprising the steps of:
- feeding data on instantaneous position as well as flight and target data into a computer onboard the guided missile, the data being fed while the guided missile is on the ground;
carrying the guided missile into the air, with the carrier airplane;
continually updating the initial data entered into the computer, after said step of feeding data, by providing changing values without cooperation from the carrier airplane, the changing values being provided from an inertial navigation system including one or more navigational aids provided onboard the guided missile, said values being further calculated for performing autonomous flight guidance and self guiding of the missile; and
maintaining a power supply onboard the guided missile beginning from the moment of data reception and continuing during a duration of a mission.
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Accused Products
Abstract
Process for the autonomous positional control of guided missiles, which are to be launched from a carrier plane, but without the cooperation thereof, wherein data on the instantaneous position of the guided missile, as well as flight and target data are fed into a computer of the guided missile already on the ground. The initial data fed into the computer are continually updated with changing values from the inertial navigation and additional navigational aids and are further calculated to achieve autonomous flight guidance and self-guiding of the missile. An uninterruptible power supply of the guided missile is maintained beginning from the moment of data reception.
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Citations
8 Claims
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1. A process for the autonomous positional control of guided missiles, the guided missiles being launched from a carrier airplane, without cooperation from the carrier airplane, the process comprising the steps of:
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feeding data on instantaneous position as well as flight and target data into a computer onboard the guided missile, the data being fed while the guided missile is on the ground; carrying the guided missile into the air, with the carrier airplane; continually updating the initial data entered into the computer, after said step of feeding data, by providing changing values without cooperation from the carrier airplane, the changing values being provided from an inertial navigation system including one or more navigational aids provided onboard the guided missile, said values being further calculated for performing autonomous flight guidance and self guiding of the missile; and maintaining a power supply onboard the guided missile beginning from the moment of data reception and continuing during a duration of a mission. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. A process for the positional control of a guided missile, the process comprising the steps of:
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providing a computer on board the guided missile and providing one or more navigational aids on board the guided missile; feeding data on instantaneous position as well as flight and target data into the computer, the data being fed while the guided missile is on the ground; connecting the guided missile to a carrier airplane and subsequent to said step of feeding data, carrying said guided missile into the air, with the carrier airplane; updating the initial data entered into the computer, said step of updating commencing after said step of feeding data and continuing while said guided missile is connected to said airplane, by providing changing positional values without interaction with the carrier airplane, the changing positional values being provided from an inertial navigation system including one of said navigational aids provided on board the guided missile; separating said guided missile from said carrier airplane and further calculating changing values for performing autonomous flight guidance and self guiding of the guided missile; and maintaining a power supply on board said guided missile, said power supply being maintained in an operational state from a time of data reception and continuing in an operational state for a duration of a mission.
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Specification