참고문헌 (17)

1. Bose, S. C. 1997, Lecture Note on GPS/INS Integrated Navigation Systems (San Diego, CA: Technalytics, Inc.) 

2. Clark, G. 2003, Angular and linear velocity estimation for a re-entry vehicle using six distributed accelerometers - Teory, simulation, and feasibility, Lawrence Livermore National Lab Technical Report, US, No. UCRL-ID-153253 

3. Doty, J. H. & McGraw, G. A. 2003, Spinning-Vehicle Navigation Using Apparent Modulation of Navigation Signals, U. S. Patent, No. 6520448B1 

4. Edwan, E., Knedlik, S., & Loffeld, O. 2011, Constrained Angular Motion Estimation in a Gyro-Free IMU, IEEE Transactions on aerospace and electronic systems, 47, 596-610. https://doi.org/10.1109/TAES.2011.5705694 

   상세보기

5. Hanson, R. & Pachter, M. 2005, Optimal Gyro-Free IMU Geometry, in AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2005-6151, Aug. 2005, San Francisco, CA. https://doi.org/10.2514/6.2005-6151 

6. Harkins, T. E. 1994, Assessing the feasibility of accelerometer-only inertial measurements units for artillery projectiles, USA Army Research Laboratory Research Reports, AR-MR-200 

7. Mickelson, W. A. 2000, Navigation system for spinning projectiles, U.S. Patent No. 6163021A 

8. Pachter, M., Welker, T. C., & Huffman Jr, R. E. 2013, Gyro-Free INS Teory, Journal of the Institute of Navigation, 60, 85-96. https://doi.org/10.1002/navi.32 

   상세보기

9. Padgaonkar, A. J., Krieger, K. W., & King, A. I. 1975, Measurement of Angular Acceleration of a Rigid Body Using Linear Accelerometers, Journal of Applied Mechanics, 42, 552-556. https://doi.org/10.1115/1.3423640 

   상세보기

10. Pamadi, K. B., Ohlmeyer, E. J., & Pepitone, T. R. 2004, Assessment of a GPS Guided Spinning Projectile Using an Accelerometer-Only IMU, in AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2004-4881, 16-19, Aug. 2004, Providence, Rhode Island. https://doi.org/10.2514/6.2004-4881 

11. Santiago, A. A. 1992, Extended Kalman Filtering Applied to a Full Accelerometer Strapdown Inertial Measurement Unit, MS Tesis, Massachusetts Institute of Technology 

12. Schuler, A. R., Grammatikos, A., & Fegley, K. A. 1967, Measuring Rotational Motion with Linear Accelerom- eters, IEEE Transactions on Aerospace and Electronic Systems, AES-3, 465-472. https://doi.org/10.1109/TAES. 1967.5408811 

    상세보기

13. Tan, C.-W. & Park, S. 2002, Design and Error Analysis of Accelerometer-Based Inertial Navigation Systems, California Partners for Advanced Transit and Highways (PATH), Institute of Transportation Studies, UC Berkeley Technical Report, UCB-ITS-PRR-2002-21 

14. Tan, C.-W., Park, S. S., Mostov, K., & Varaiya, P. 2001, Design of Gyroscope-Free Navigation Systems, IEEE Intelligent Transportation Systems Conference, 25-29 Aug. 2001, Oakland, CA, USA, pp.286-291. https://doi. org/10.1109/ITSC.2001.948670 

15. Titterton, D. & Weston, J. L. 2004, Strapdown Inertial Navigation Technology, 2nd Ed. (AIAA: Reston) 

16. Wei, M. & Schwarz, K. P. 1990, A Strapdown Inertial Algorithm Using Earth-Fixed Cartesian Frame, Navigation: Journal of The Institute of Navigation, 37,153-167. https://doi. org/10.1002/j.2161-4296.1990.tb01544.x 

17. Wray, G. L. & Flynn, D. J. 1979, An Assessment of Various Solutions of the Navigation Equation for a Strapdown Inertial System, Technical Report 79017, Royal Aircraft Establishment 

저자의 다른 논문 :

Lee, Junhak (1) Kim, Heyone (1) 황동환 (51) 이상정 (160)