http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2001108737-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5547f741b25666fc4ae5195cf71a979b |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01S7-38 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B12-70 |
| filingDate | 1999-10-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d80c51bd8e77522b15b1077db658834f http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a74c78adce0442bf4a3f25c196b8b7da http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bc94fcb6398bbdf32a377007ad1ceeda |
| publicationDate | 2001-04-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2001108737-A |
| titleOfInvention | Radar system |
| abstract | (57) [Summary] [Problem] To transmit a pseudo radio wave when a decoy constituting a decoy device for guiding an ARM using a plurality of decoys is broken or destroyed and only one decoy for transmitting a pseudo radio wave is provided. The decoy will surely be destroyed by the ARM. On the other hand, by always knowing the state of failure or destruction of the decoy and changing the control method of the ARM guidance when the decoy is broken or destroyed, it is possible to avoid the destruction of the radar device by the ARM and to keep the decoy device remaining. To provide a radar system for improving performance. The status of two decoys 3 and 4 of a decoy device 2 is constantly monitored by a decoy operation monitor 18, and when one of the decoys is broken down or destroyed, a decoy operation selector 14 and a decoy operation controller 15 are used. The control method of the decoy device 2 is switched, and the transmission of the pseudo radio wave from the decoy is stopped at the predicted time when the ARM 31 reaches the preset distance. By stopping the transmission of the decoy device 2, the flight method of the ARM 31 to the target is changed from the radio homing flight to the inertial flight, and the landing on the target is dispersed. |
| priorityDate | 1999-10-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.