Study on models of gyroscope-free strap-down inertial navigation system

Binggong Xuebao/Acta Armamentarii

Volumn 27, Issue 2, 2006, Pages 288-292

  Wang, Xiao Na ^a   Wang, Shu Zong ^a   Zhu, Hua Bing ^a  

^a NAVAL UNIVERSITY OF ENGINEERING   (China)

Author keywords

Accelerometer; Configuration; Control and navigation for fligh vehicle; Gyroscope free strap down inertial navigation

Indexed keywords

ACCELEROMETERS; AIRCRAFT; ALGORITHMS; COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; GRAVITATIONAL EFFECTS; GYROSCOPES; SENSORS; VELOCITY;

ANGULAR VELOCITY; CARRIER MOTION; CONFIGURATION; GYROSCOPE FREE STRAP DOWN INERTIAL NAVIGATION;

INERTIAL NAVIGATION SYSTEMS;

EID: 33745139528     PISSN: 10001093     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

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2. YIN De-jin, WANG Hong-li, LIU Guang-bin. 6-accelerometer configuration scheme for SINS[J]. Journal of Chinese Inertial Technology, 2003, (2): 48-51. (in Chinese)
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5. CHEN Zhe. Principles of strap-down inertial navigation systems[M]. Beijing: China Astronautics Publishing House, 1986: 40-43. (in Chinese)