Design of a low-cost attitude determination GPS/INS integrated navigation system

Author:

Hwang Dong-Hwan,Oh Sang Heon,Lee Sang Jeong,Park Chansik,Rizos Chris

Publisher

Springer Science and Business Media LLC

Subject

General Earth and Planetary Sciences

Reference30 articles.

1. Anderson RS, Hanson DS, Kourepenis AS (2001) Evolution of low-cost MEMS inertial system technologies. In: Proceedings of ION GPS 2001, The Institute of Navigation, Salt Lake City, pp 545–555

2. Arshal G (1987) Error Equations of Inertial Navigation. J Guid Control Dynam 10(4):351–358

3. Beser J, Alexander S, Crane R, Rounds S, Wyman J (2002) TRUNAV: a low-cost guidance/navigation unit integrating a SAASM-based GPS and MEMS IMU in a deeply coupled mechanization. In: Proceedings of ION GPS 2002, The Institute of Navigation, Alexandria, pp 545–555

4. Biezad DJ (1999) Integrated navigation and guidance systems. American Institute of Aeronautics and Astronautics, Reston

5. Blakelock JH (1991) Automatic Control of Aircraft and Missiles, 2nd edn. Wiley, New York

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