최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기Journal of Positioning, Navigation, and Timing, v.7 no.2, 2018년, pp.91 - 103
Lee, Junhak (Department of Electronics Engineering, Chungnam National University) , Kim, Heyone (Department of Electronics Engineering, Chungnam National University) , Oh, Sang Heon (Navcours Co. Ltd) , Do, Jae Chul (Hanwha Co.) , Nam, Chang Woo (Hanwha Co.) , Hwang, Dong-Hwan (Department of Electronics Engineering, Chungnam National University) , Lee, Sang Jeong (Department of Electronics Engineering, Chungnam National University)
Conventional inertial measurement units cannot be used in the spinning vehicle with high rotation rate due to gyro's narrow operation range. By the way, angular acceleration can be measured using the accelerometer array distributed in the vehicle. This paper derives a mechanization for the gyro-free...
Bose, S. C. 1997, Lecture Note on GPS/INS Integrated Navigation Systems (San Diego, CA: Technalytics, Inc.)
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
Doty, J. H. & McGraw, G. A. 2003, Spinning-Vehicle Navigation Using Apparent Modulation of Navigation Signals, U. S. Patent, No. 6520448B1
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
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
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
Mickelson, W. A. 2000, Navigation system for spinning projectiles, U.S. Patent No. 6163021A
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
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
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
Santiago, A. A. 1992, Extended Kalman Filtering Applied to a Full Accelerometer Strapdown Inertial Measurement Unit, MS Tesis, Massachusetts Institute of Technology
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
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
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
Titterton, D. & Weston, J. L. 2004, Strapdown Inertial Navigation Technology, 2nd Ed. (AIAA: Reston)
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
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
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
출판사/학술단체 등이 한시적으로 특별한 프로모션 또는 일정기간 경과 후 접근을 허용하여, 출판사/학술단체 등의 사이트에서 이용 가능한 논문
※ AI-Helper는 부적절한 답변을 할 수 있습니다.