¹«±â Åä·Ð¹æ
¹ÌÀ°±º Â÷±â Çï±â DTED žÀç °ü·Ã
ÀÛ¼ºÀÚ : erorist(211.253.xxx.xxx)
ÀÔ·Â 2020-05-14 11:33:04
  • Á¶È¸¼ö 3095
  • ´ñ±Û 0
  • Ãßõ 0 print
¹ÌÀ°±ºÀº Â÷±âÇï±â¸¦ °³¹ßÁßÀε¥ ÀÛÀü¿ä±¸»çÇ×À» ¿©·¯°¡Áö ¹Ý¿µ ¿ä±¸ÇÏ°í ÀÖ½À´Ï´Ù
Â÷±âÇï±â Áß¿¡´Â FARA¶ó°í Â÷±âÁ¤ÂûÇï±â°¡ Àִµ¥ ¾Ë·¹À̹öÅ© °Ý³³°í¿¡ µé¾î°¡´Â Å©±â·Î ¿ä±¸ÇÏ°í ÀÖ°í DTED(½Ç½Ã°£ Á¤¹Ð ÁöÇü´ëÁ¶Ç×¹ý) žÀç°¡ ¿ä±¸µË´Ï´Ù
DTED´Â µðÁöÅÐ ÁöÇü°íµµ µ¥ÀÌÅͶó´Â Àǹ̷ΠÁö¿ÀÀ̵å Æò¸éÀÇ °íµµº° ÁöÇüÁö¹° µ¥ÀÌÅÍ°ªÀ» µðÁöÅÐ Áöµµ·Î Ç¥ÇöÇÑ µ¥ÀÌÅͺ£À̽º¸¦ ¸»ÇÕ´Ï´Ù Áï DTED¸¦ ÀåÂøÇϸé GPS°¡ ¾ø¾îµµ ÀÌ Àåºñ¸¸À¸·Î GATM/EGI¿Í ¿¬µ¿ÇÏ¿© ¿øÇÏ´Â °÷À¸·Î ºñÇàÇÒ ¼ö ÀÖ½À´Ï´Ù ÀûÀÇ GPSÀç¹Ö»óȲ¿¡ °¡Àå Áß¿äÇÑ ÀåºñÀÔ´Ï´Ù

Sensors: 360µµ ½Ã¾ßÀÇ STARING ARRAY(GaN AESA, EOIR, MMW MIMO imaging?), °øÁß¼± ½Äº°±â´É µîÀ» °®Ãâ °Í, ¸ðµç ¼¾¼­ Á¤º¸´Â HUD¿¡ Àü¼ÛÇÒ ¼ö ÀÖÀ» °Í
Sensor systems and fused sensor systems capable of providing pilotage through a solid state staring array covering 360 degrees in degraded visual environments (DVE), day/night air and ground targeting at close, mid, and extended ranges to maximize target acquisition capabilities and support all munition types, low-light and wire/obstacle detection, radar detection, radar interferometry, weather detection, terrain avoidance, and situational awareness. Software that minimizes pilot workload through fusion of multiple sensor inputs and artificial intelligence to aid in pilot decision-making. All sensor data should be capable of internal transmission to pilot head-up displays and multiple cockpit displays and external transmission to other systems in the operational environment.
 Communications: SATCOM°ú ¸µÅ©16À» °®Ãâ °Í, IFF M5L2 out/in, ADS-B in/out
A multi-band and single band communications suite capable of providing line of sight and beyond light of sight communications in HF, VHF (AM/FM), UHF (AM/SATCOM), Link 16, advanced networking waveforms, Blue Force Tracking, workload-reduced manned/unmanned (MUM) teaming through Level of Interoperability (LOI) 5, identification/transponders, and internal communications. Aircraft Surveillance capable of Mode 5 Level 2 out/in, Mode 5 Level 2 Broadcast, Automatic Dependent Surveillance Broadcast (ADS-B) In/out, and interrogation of air and ground threats. The FARA PM is interested in a comprehensive suite that minimizes weight, simplifies integration for future modifications/upgrades, and is fully integrated with and conformant to the aircraft open system architecture.
Navigation: TACAN/DTED¸¦ °®Ãâ °Í
Aircraft navigation sets capable of legacy and next generation civil navigation modes in VHF Nav/ILS, TACAN, Doppler, EGI with M-code encryption, and assured precision navigation and timing (A-PNT), and Digital Terrain Elevation Data (DTED) assisted visual-based solutions for aerial navigation in GPS denied environments and under Instrument Meteorological Conditions (IMC). The FARA PM is also interested in solutions and software applications that support supervised autonomy / optionally-manned flight.
Survivability: GFAS °°Àº Àåºñ °®Ãâ °Í
Aircraft Survivability Equipment to provide spherical coverage of the host platform in order to defeat the FARA threats. Aircraft survivability systems capable of detecting RF, IR, and laser threats. Missile warning systems capable of threat launch detection. Hostile fire systems capable of ballistic fire detection. Countermeasure systems capable of protecting against RF and IR threats. Electronic Warfare (EW) to include RF jamming systems. The FARA PM is interested in a comprehensive ASE suite that minimizes weight, can be fused with aircraft navigation and pilotage systems, and fully integrated with and conformant to the aircraft open architecture.
Infrastructure / Digital Backbone: Components, technologies and standards that support and complement the Government¡¯s MOSA objective to enable rapid development, integration, and modification of mission systems and enhanced mission systems capabilities by qualified third-party integrators without air vehicle OEM involvement.
Data Fusion: Technology that enables fusion of multiple aircraft data inputs to support creation of a synthetic operating picture to improve mission effectiveness and reduce crew workload.
Pilot Interface: Heads up / helmet mounted displays that are high definition, color-capable, and night-vision device compatible. Cognitive decision aiding tools such as voice activation technology, 3D audio, and other cueing capabilities.
Effectors: Fully-integrated 20mm cannon with minimum 180 degree, desired 360 degree of azimuthal coverage and 60 degree elevation coverage.


´ñ±Û
0 / 500
Top