System, method, and computer program product for hostile fire strike indication
US-2015377709-A1 · Dec 31, 2015 · US
US10082367B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10082367-B2 |
| Application number | US-201414898170-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 12, 2014 |
| Priority date | Jun 14, 2013 |
| Publication date | Sep 25, 2018 |
| Grant date | Sep 25, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of conducting a strike against a target using a designator and a missile. The following steps are conducted: (i) the designator designates the target using a first signal, such as a laser; (ii) the missile detects the laser reflected off the target; (iii) after detecting the reflected laser, the missile emits a second signal, such as a LADAR signal, to designate the target; (iv) the missile tracks the so-designated target; (v) the designator detects the LADAR signal reflected off the target; and (vi) in response to detecting the reflected LADAR signal, the designator stops the designation of the target. This may enable the designator to perform other tasks, while the missile tracks and engages the target.
Opening claim text (preview).
The invention claimed is: 1. A method of conducting a strike against a target using a designator and a missile, in which method the following steps are conducted: (i) the designator designates the target using a first signal; (ii) the missile detects the first signal reflected off the target; (iii) after detecting the reflected first signal, the missile emits a second signal to designate the target; (iv) the missile tracks the so-designated target; (v) the designator detects the second signal reflected off the target; and (vi) having detected the reflected second signal, the designator stops designating the target using the first signal, thereby enabling the designator to perform other tasks, whilst the missile tracks and engages the target. 2. A method according to claim 1 , wherein the second signal is encoded with information, and step (vi) comprises decoding the second signal to read the information. 3. A method according to claim 1 , wherein the second signal is a laser signal. 4. A method according to claim 1 , wherein the second signal is a LADAR signal. 5. A method according to claim 4 wherein the second signal is a scanning LADAR signal. 6. A method according to claim 1 wherein in step (iv) the designated target is tracked using the second signal. 7. A method according to claim 1 , wherein the first signal is a laser signal. 8. A method according to claim 1 , wherein the first signal is encoded with information, and wherein the method comprises the step of decoding the first signal. 9. The method according to claim 1 , further including the missile including information in the second signal indicating that the missile has designated the target. 10. The method according to claim 9 , wherein step (vi) includes in response to the designator detecting that the reflected second signal contains information indicating that the missile has designated the target, the designator stops designating the target using the first signal. 11. The method according to claim 10 , further including the designator including information in the first signal indicating that the designator is aware that the missile has designated the target and will stop sending the first signal. 12. The method according to claim 11 , further including the missile detecting that the first signal contains information indicating that the designator will stop sending the first signal. 13. A target designating system comprising: a designator comprising: (a) a laser source for emitting a first laser signal for designating a target, (b) a detector for detecting a reflection of a second signal; and (c) a decoder for decoding the reflection of second signal; and a first missile comprising: (A) an encoder for encoding the second signal, (B) a source for emitting the second signal, (C) a detector for detecting the reflection of the first signal and for detecting a reflection of the second signal, and (D) a guidance system switchable between guiding the first missile to the target in a first mode that is dependent on the detection of the reflection of the first signal, and in a second mode that is dependent on the detection of the reflection of the second signal. 14. The target designating system according to claim 13 , the encoder in the first missile being arranged to encode the second signal with information. 15. The target designating system according to claim 13 , wherein the designator comprises an encoder to encode the first signal with information, and the first missile comprises a decode to decode the first signal. 16. The target designating system according to claim 13 , wherein the second signal is a LADAR signal. 17. The target designating system according to claim 13 , wherein the designator is a second missile. 18. The target designating system according to claim 13 , wherein the target is a ground target.
using electromagnetic waves other than radio waves · CPC title
using a target illuminator · CPC title
Combinations of different guidance systems · CPC title
Systems determining position data of a target · CPC title
Active homing systems, i.e. comprising both a transmitter and a receiver · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.