HOME > Á¦Ç°¼Ò°³ > CAST Navigation > GPS Simulator Support Tools
CAST 170 Terrain Obscuration Program (TOP)
TOP ¼ÒÇÁÆ®¿þ¾î´Â GPS ¼ö½Å±â¸¦ µÑ·¯½Ñ ÁöÇüÀ» ÇØ¼®Çϱâ À§ÇÑ À§¼ºÀÇ °¡½Ã¼ºÀ» ½Ç½Ã°£À¸·Î °Ë»ç Á¦°øÇÕ´Ï´Ù.
+ System Features
- Color-coded satellite visibility status for easy viewing.
- Displays terrain altitude at location of vehicle and terrain altitudes surrounding the vehicle.
- Unique 3-D visualization option for viewing the area terrain in real time.
- Equipped with Digital Terrain Elevation Data (DTED) Level 0 terrain data.
- Designed to accept higher resolution DTED data (available to authorized users only).
CAST 110 Interference Generation System
´Üµ¶¸ðµå ¶Ç´Â CAST ½Ã¹Ä·¹ÀÌÅÍÀÇ º¸¿ÏÀ» À§ÇØ »ç¿ëµË´Ï´Ù. ´Üµ¶À¸·Î »ç¿ëµÉ °æ¿ì ½Ã½ºÅÛÀº GPS ¼ö½Å±âÀÇ anti-jam ¼º´ÉÀ» Å×½ºÆ®Çϱâ À§ÇÑ ¹Ýº¹ÀûÀÎ Áö¿øÀ» Á¦°øÇÕ´Ï´Ù. »ç¿ëÀÚ´Â ±¤´ë¿ª, Çù´ë¿ª ÀüÆÄ¿¡ ´ëÇÑ ¹æÇØ ·¹º§°ú ½ÅÈ£ Àü¼Û Ư¼ºÀ» ÁöÁ¤ÇÒ ¼ö ÀÖ½À´Ï´Ù.
+ System Features
- Jammer configurations are defined prior to execution and are
  associated with scenarios stored on the simulator.
- During scenario execution, the jammer and GPS RF signals are
  generated and transmitted together as a composite signal.
- Each jammer can be assigned an initial speed, altitude and
  stationary or dynamic trajectory profile.
- A programmable jamming signal source is commanded in real time
  as canned scenarios fly a particular flight path or as a flight path is
  defined externally using an aircraft model.
CAST 100 GPS Monte Carlo Navigation Simulator (NAVSIM)
NAVSIMÀº Global Positioning System(GPS)°úInertial Measurement Unit(IMU)ÀÇ Á¾ÇÕÀûÀÎ Monte Carol SimulationÀÔ´Ï´Ù NAVSIMÀº ½Ã½ºÅÛ ±¸¼º ¼±ÅÃ, ½Ã½ºÅÛ Æ©´×, Sensor tradeoff ¿¬±¸, ½Ã³ª¸®¿À Áغñ ¹× ¼º´É ºÐ¼®¿¡ µµ¿òÀ» ÁÖ±â À§ÇÑ ºÐ¼® µµ±¸ÀÔ´Ï´Ù.
+ System Features
- Set vehicle type and simulated dynamics, sensor variables, INS error
  parameters, GPS receiver configuration, and satellite constellation
   parameters.
- Interactively tailor a vehicle motion profile and selectively control satellite
  signal reception and degradation.
- Perform actual Monte Carlo simulation of GPS/INS system based on
  parameters you provide including data rates, navigation profile, Kalman
  filter processing, and hardware configuration.
- Configure the GPS receiver as a navigation subsystem for providing
  position and velocity data.
- Control a complete set of avionic sensors in addition to GPS
  measurements.
- Compute navigation error statistics, print reports of analysis, and view
  plots of selected error statistics.
- System is installed on Pentium¢ç-based Windows PC.
- Hardware-in-the-loop option available.