A low cost integrated navigation system applied on UAV and some simulations results

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 7128, Issue , 2008, Pages

  Liu, Wei ^a   Zhang, Jingjuan ^a   Yang, Guoliang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Dead reckoning; Heading calibration; Kalman filtering; UAV

Indexed keywords

COMPASSES (MAGNETIC); CONTROL THEORY; INSTRUMENTS; LAUNCHING; MEASUREMENT THEORY; NAVIGATION; UNMANNED AERIAL VEHICLES (UAV);

AERIAL VEHICLES; AIRBORNE EQUIPMENTS; DEAD RECKONING; DEAD RECKONINGS; DIVERGENT TRENDS; HEADING CALIBRATION; INTEGRATED MEMS; INTEGRATED NAVIGATION SYSTEMS; KALMAN FILTERING; LOW COSTS; MAGNETIC COMPASSES; UAV;

NAVIGATION SYSTEMS;

EID: 56249087940     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.806881     Document Type: Conference Paper

References (3)

1. Yi Guangqu, Inertial Navigation Principle, Aviation Industry Press, Beijing, 1987.
2. Wang Huinan, Principles and Applications of GPS Navigation, Scientific Press, Beijing, 2003.
3. Lin Xueyuan, Liu Huazhang and Shi Pei, "One GPS / SINS of Low Cost and Low Precision Integrated Navigation System and Its Experiments," Journal of Wuhan University(natural science edition), Vol. 31 No. 10 Oct . (2006).