Stealth weapon systems
OwnerRaymond C. Mortoninventor
Life of this patent
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Abstract
A winged bomb is launched from a launch aircraft and glides to a target. During the glide the winged bomb follows a calculated guide path stored in a on board computer, with correction generated by the computer using data from an altimeter and global positioning receiver. Near the termination of the glide a television camera is activated and transmits signals to a remote location from which final correction are manually generated and transmitted by radio to the bomb. The bomb is designed with low radar cross section.
Claims11
The method of utilizing a winged bomb which is maneuverable by control surfaces comprising:
- a) loading the winged bomb onto a launch aircraft,
- b) inputting data in the aircraft to a computer program for a calculated glide path of the bomb from the aircraft to a target,
- c) transferring the calculated guide path program to a bomb computer on board the bomb, then
- d) releasing the bomb from the aircraft, and
- e) guiding the bomb along the calculated glide path using the program with the inputted data.
The method of utilizing a winged bomb which is maneuverable by control surfaces comprising:
- a) loading the winged bomb onto a launch aircraft,
- b) inputting data in the aircraft to a computer program for a calculated glide path of the bomb from the aircraft to a target,
- c) transferring the calculated guide path program to a bomb computer on board the bomb, then
- d) releasing the bomb from the aircraft,
- e) guiding the bomb along the calculated glide path using the program with the inputted data ,
- f) deploying wings on the bomb after the bomb is released from the aircraft,
- g) periodically entering data on the bomb computer of a determined position of the bomb by
- h) reading an altimeter on the bomb, and
- i) reading the geographic position of the bomb from data derived from a global positioning satellite receiver on the bomb, then
- j) correcting any deviation of the determined position of the bomb from the calculated glide path position, by
- k) producing a correction on the bomb computer of the deviation from the calculated path,
- l) changing the control surfaces responsive to the correction,
- m) at a predetermined distance from the target on the bomb computer's calculated guide path, creating television signals by activating a television camera on the bomb, directed at the target,
- n) transmitting the television signals to a control aircraft,
- o) displaying and recording the view shown by the television signals in the control aircraft,
- p) manually producing overriding control signals in the control aircraft,
- q) transmitting the overriding signals to the bomb,
- r) guiding the bomb by the overriding signals,
- s) said calculated glide path is for a bomb flight of a maximum distance of ten (10) times the aircraft altitude at the time of the launch, and
- t) said calculated guide path is for a bomb flight of a distance at least equal to the aircraft altitude at the time of the launch.
Dependencies are inferred from the claim text.