Patent ID: 8798812

Claim:
A three-dimensional (3D) digital map system comprising: a Terrain Referenced Navigation (TRN) module configured to receive data from EGI (Embedded GPS/INS), a radio-altimeter (RALT) and a map database, correct the data to perform accurate navigation computation, and output the corrected data; wherein the TRN module includes: a data synchronization function configured to internally store information received from the EGI and the radio-altimeter through a time tag; a Bayesian filter configured to estimate a current latitude and longitude of the aircraft using the data synchronized by the data synchronization function and Digital Terrain Elevation data (DTED); a Kalman filter configured to receive the estimated latitude and longitude and correct aircraft status data of the EGI; and a switch configured to check the estimation state of the Kalman filter and bypass the data of the EGI or output the data of the EGI corrected by the Kalman filter; a Collision Avoidance Warning (CAW) module configured to generate a warning against collision of an aircraft with the ground or an obstacle using the corrected data, a 3D terrain database and an obstacle database; wherein the CAW module includes: an aircraft prediction trajectory generation module configured to receive maximum allowable load coefficient information outputted from a flight control module; a near terrain generation module configured to receive high-resolution satellite image terrain data stored in a Digital Moving Map (DMM) module, data of an obstacle database and data of an anti-air threat database; a search range setting module configured to receive the latitude, longitude, height and velocity of the aircraft and attitude information of the aircraft, which are outputted from a navigation system, set a search range, and output the information to the near terrain generation module or the aircraft prediction trajectory generation module; a terrain-and-trajectory comparison module configured to receive and analyze the data of the databases and the aircraft status outputted from the near terrain generation module and the aircraft prediction trajectory generation module: and a status recognition module configured to output various warnings according to the analyzed data of the databases and aircraft status; a Terrain Following (TF) module configured to generate a terrain following trajectory of the aircraft using the corrected data, the 3D terrain database and the obstacle database: wherein the TF module further includes an excess thrust computation module configured to determine a maximum climbing rate, a constant-slope module for simplifying a terrain, and a moving average module considering a turn rate; and a Passive Ranging (PR) module configured to receive the 3D terrain database and line-of-sight (LOS) information of a target and calculate distance and position information of the target located on the ground; wherein the PR module further includes a line-of-sight ranging module and a coordinate ranging module.