JDAM and similar applications impose meter-level error budgets on navigation. Validation in the military flight envelope is challenging and expensive. Existing carrier phase truth systems are capable of decimeter performance, but fail in realistic maneuvers and blockages. In Phase I, TISI overcame these problems by processing raw baseband data from all satellites in a powerful adaptive filter structure. Patented, this is known as Integrated Demodulation/Navigation (IDN). Simulations were performed with single and multiple antennas, with and without IMU, in figure 8, dive, and aileron roll maneuvers up to 18gs. Optimal combining of dual antennas mitigated satellite blockage. Instabilities encountered in tightly coupled GPS/IMU configurations were eliminated. The algorithm combines its robust 100 Hz carrier phase data with host 10 Hz P-code pseudoranges , to produce decimeter navigation quality. In phase II, a demonstration processor will be developed in tree stages: a desktop standalone version with IMU, a desktop version interfaced with HDIS, and a PC-104 format version interfaced with HDIS. Off- the-shelf board level components are utilized. Extensive RF simulations and vehicle tests are scheduled. The final task feasibility study of a directly embedded IDN algorithm within the host.
Benefit: Improvements in the blockage, multipath, jamming and spoofing are urgently needed by many user segments. The algorithms and processor developed here are the basis of a new generation of robust decimeter systems, meeting the needs of a large and rapidly growing civilian military DGPS market.
Keywords: Algorithms, DGPS, Processor, Modular, Carrier, aiding, phase, IMU