US4234141A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Range gated retroreflective missile guidance system
Assignee: United States Department of the Army
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Filing: 1970-03-10
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Granted: 1980-11-18
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Expires: 1990-03-10
Abstract
Abstract An optical tracking link in an automatic command to line-of-sight missile idance system improves the system efficiency and employs a reuseable light source. In tracking a missile during trajectory toward a target, short pulses of collimated light are transmitted from the launch site toward the missle. These light pulses are received by a missile optical receiver for guidance of the missile and are simultaneously reflected by a retrodirective prism on the missile. The reflected energy follows a path parallel to the incident wave and is thus directed back to the launch site. A missile tracker at the launch site responds to the reflective energy, measuring any deviation of the missile from a line-of-sight axis maintained between the launch site and a target. Guidance commands are transmitted toward the missile for maintaining the missile on the line-of-sight trajectory and containing correctional signals in response to any missile deviation. During intervals between return reflections, the missile tracker can be gated off. This greatly reduces background and jamming source reflections and signals, received by the tracker providing effective counter measures hardening of the system.
Inventors
- 👤 Walter E. Miller, Jr.
- 👤 Jimmy R. Duke
- 👤 George W. Starkey
- 👤 Robert L. Sitton
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 10:05
CPC Classifications
F; F41; F41G; F41G7/00; F41G7/20; F41G7/30
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
119 words
A range gated retroreflective guidance system for a missile system comprising: an optically sensitive receiver within the housing of a missile to be tracked for command control of said missile, a tracking station having an optical transmitting means for transmitting a periodic burst of light energy toward said missile optical receiver for providing a missile guidance signal, a telescope at said tracking station for maintaining directional alignment between said target and said tracking station, optically sensitive missile tracking means at said tracking station for following the direction of flight of a missile, and a retrodirective corner-cube prism adjacent said optical receiver for reflecting a portion of said optically transmitted guidance signal from said missile to said optical tracking means.
Claim 2
Dependent Claim
119 words
A range gated retroreflective guidance system for a missile system comprising: an optically sensitive receiver within the housing of a missile to be tracked for command control of said missile, a tracking station having an optical transmitting means for transmitting a periodic burst of light energy toward said missile optical receiver for providing a missile guidance signal, a telescope at said tracking station for maintaining directional alignment between said target and said tracking station, optically sensitive missile tracking means at said tracking station for following the direction of flight of a missile, and a retrodirective corner-cube prism adjacent said optical receiver for reflecting a portion of said optically transmitted guidance signal from said missile to said optical tracking means.
Claim 3
Dependent Claim
21 words
A range gated retroreflective guidance system as set forth in claim 1 wherein said optical transmitting means is a gallium-arsenide laser.
Claim 4
Dependent Claim
64 words
A range gate retroreflective guidance system as set forth in claim 2 wherein said optically sensitive tracking means comprises an optical detector coaxial to said light emitting transmitter, and a gating circuit for activating said optical detector only during periods of anticipated energy return and for providing an increasing variable delay between the activation of said transmitter and the gating on of said receiver.
Claim 5
Independent Claim
215 words
A method for providing a range gated retroreflective guidance system between a missile and a relatively fixed tracking station, said tracking station being disposed for distinguishing a target and maintaining said missile on a trajectory terminating at said target, comprising the steps of: (a) maintaining said target in a line-of-sight relationship with an observer at said tracking station, (b) directing an output signal of optical energy from said tracking station toward said missile during traversal of said trajectory, (c) receiving said signal of optical energy by said missile, (d) reflecting a portion of said received optical energy signals from a corner-cube prism on said missile to said tracking station along a path substantially parallel with the path of incidence in immediate response to said received signal, (e) receiving and detecting the reflected optical energy by said tracking station for tracking said missile in the trajectory toward said target, (f) re-directing output signals of optical energy from said tracking station toward said missile for correcting and maintaining the relative position of said missile in the trajectory toward said target, and (g) generating attitude responses within said missile in proportion to relative displacement between the missile and said line-of-sight for retention of said missile in trajectory in response to said tracking station directing and re-directing output signals.
Claim 6
Independent Claim
215 words
A method for providing a range gated retroreflective guidance system between a missile and a relatively fixed tracking station, said tracking station being disposed for distinguishing a target and maintaining said missile on a trajectory terminating at said target, comprising the steps of: (a) maintaining said target in a line-of-sight relationship with an observer at said tracking station, (b) directing an output signal of optical energy from said tracking station toward said missile during traversal of said trajectory, (c) receiving said signal of optical energy by said missile, (d) reflecting a portion of said received optical energy signals from a corner-cube prism on said missile to said tracking station along a path substantially parallel with the path of incidence in immediate response to said received signal, (e) receiving and detecting the reflected optical energy by said tracking station for tracking said missile in the trajectory toward said target, (f) re-directing output signals of optical energy from said tracking station toward said missile for correcting and maintaining the relative position of said missile in the trajectory toward said target, and (g) generating attitude responses within said missile in proportion to relative displacement between the missile and said line-of-sight for retention of said missile in trajectory in response to said tracking station directing and re-directing output signals.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-11-18 | 1984-05-19 | 1984-11-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-11-18 | 1988-05-19 | 1988-11-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-11-18 | 1992-05-19 | 1992-11-18 | $7700.00 | Window Closed / Lapsed |