| 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. |
|
 |
|
|