WANG Huinan, HE Feng. REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE[J]. Chinese Journal of Space Science, 1998, 18(1): 69-74. doi: 10.11728/cjss1998.01.069
Citation:
WANG Huinan, HE Feng. REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE[J]. Chinese Journal of Space Science, 1998, 18(1): 69-74. doi: 10.11728/cjss1998.01.069
WANG Huinan, HE Feng. REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE[J]. Chinese Journal of Space Science, 1998, 18(1): 69-74. doi: 10.11728/cjss1998.01.069
Citation:
WANG Huinan, HE Feng. REAL-TIME KINEMATIC ATTITUDE DETERMINATION OF AIRCRAFT USING GPS CARRIER PHASE[J]. Chinese Journal of Space Science, 1998, 18(1): 69-74. doi: 10.11728/cjss1998.01.069
The paper describes the basic idea of real-time attitude determination using GPS carrier phase and introduces a mathematical model for attitude determination system. The paper presents an effcient method for resolving single difference phase ambiguities and reveals the meanings of the physics by nature.