1 |
Schuler, A. R., Grammatikos, A., & Fegley, K. A. 1967, Measuring rotational motion with linear accelerometers, IEEE Transactions on Aerospace and Electronic Systems, AES-3, 465-472. https://doi.org/10.1109/TAES.1967.5408811
DOI
|
2 |
Septentrio 2009, AsteRx2eH: GPS/GLONASS Dual-frequency Heading receiver, SSNDS 09/2009/17. http://www.formosatrend.com/Precision_SUM.html
|
3 |
Son, J. H., Oh, S. H., & Hwang, D.-H. 2020, Design of loosely-coupled GPS/GF-INS integrated navigation algorithm, 2020 IPNT Conference, Yeosu, 11-13 Nov 2020.
|
4 |
Swift Navigation 2019, Piksi Multi, GNSS Module Hardware Specification, 000-534-02-02. https://www.swiftnav.com/piksi-multi
|
5 |
Sorrentino, F., Lien, Y., Rosi, G., Cacciapuoti, L., Prevedelli, M., & Tino, G. 2010, Sensitive Gravity- Gradiometry with Atom Interferometry: Progress Towards an Improved Determination of the Gravitational Constant, New Journal of Physics, 12, 1-16. https://doi.org/10.1088/1367-2630/12/9/095009
DOI
|
6 |
McGuirk, J. M., Foster, G. T., Fixler, J. B., Snadden, M. J., & Kasevich, M. A. 2002, Sensitive Absolute-Gravity Gradiometry Using Atom Interferometry, Physics Review A, 65, 1-14. https://doi.org/10.1103/PhysRevA.65.033608
DOI
|
7 |
Tan, C.-W. & Park, S. 2005, Design of Accelerometer-Based Inertial Navigation Systems, IEEE Transactions on Instrumentation and Measurement, 54, 2520-2530. https://doi.org/10.1109/TIM.2005.858129
DOI
|
8 |
Titterton, D. H. & Weston, J. L. 2004, Strapdown Inertial Navigation Technology, 2nd Ed. (Stevenage: The Institute of Electrical Engineers)
|
9 |
u-blox 2015, NEO-7 series - u-blox 7 GNSS modules, product information, UBX-13003342-R07. https://www.u-blox.com/en/product/neo-7-series
|
10 |
u-blox 2021, NEO-M8 - u-blox M8 concurrent GNSS modules Data sheet, UBX-15031086-R11. https://www.u-blox.com/en/product/neo-m8-series
|
11 |
Qin, Z., Baron, L., & Birglen, L. 2009, Robust design of inertial measurement units based on accelerometers, Journal of Dynamic Systems Measurement and Control, 131, 1-10. https://doi.org/10.1115/1.3072157
DOI
|
12 |
Honeywell 2021, GG1320AN Digital Laser Gyro, Brochure: GG1320AN Digital Ring Laser. https://aerospace.honeywell.com/us/en/learn/products/sensors/gg1320an-digital-ring-laser-gyroscope
|
13 |
Chen, J. H., Lee, S.-C., & Debra, D. B. 1994, Gyroscope free strapdown inertial measurement unit by six linear accelerometers, Journal of Guidance, Control, and Dynamics, 17, 286-290. https://doi.org/10.2514/3.21195
DOI
|
14 |
Edwan, E., Knedlik, S., Zhou, J., & Loffeld, O. 2009, GPS/INS integration for GF-IMU of twelve mono-axial accelerometers configurations, in the 6th Workshop on Positioning, Navigation, and Communication 2009(WPNC' 09), Hannover, Germany, 19 Mar 2009. https://doi.org/10.1109/WPNC.2009.4907825
DOI
|
15 |
Honeywell 2004, Q-FLEX QA-2000 ACCELEROMETER, The inertial navigation standard, N61-2509-000-000. https://aerospace.honeywell.com/us/en/learn/products/ sensors/qa-2000-single-axis-quartz-accelerometer
|
16 |
Klein, I. 2015, Analytic error assessment of gyro-free INS, Journal of Applied Geodesy, 9, 49-61. https://doi.org/10.1515/jag-2014-0015
DOI
|
17 |
Li, Y., Zhang, K., Roberts C., Murata, M. 2004, On-the-fly GPS-based attitude determination using single and double- differenced carrier phase measurements, GPS Solutions, 8, 93-102. https://doi.org/10.1007/s10291-004-0089-3
DOI
|
18 |
Liu, F., Su, Z., Zhao, H, Li, Q., & Li, C. 2019, Attitude Measurement for High-Spinning Projectile with a Hollow MEMS IMU Consisting of Multiple Accelerometers and Gyros, Sensors, 19, 1799. https://doi.org/10.3390/s19081799
DOI
|
19 |
Moon, J. 2014, Design of a Real-time GPS Attitude Determination System using Low-cost GPS Receivers, M.S. Thesis, Chungbuk National University. https://cbnul.chungbuk.ac.kr/search/DetailView.ax?sid=1&cid=2536291
|
20 |
Marques Filho, E. A., Kuga, H. K., & Neto, A. R. 2006, Integrated GPS/INS Navigation System Based on a Gyroscope-Free IMU, in DINCON 2006: Brazilian Conferenceon Dynamics, Control and Their Applications, Guaratingueta, SP, Brazil, 22-26 May 2006
|
21 |
Nusbaum, U. & Klein, I. 2017, Control theoretic approach to gyro-free inertial navigation systems, IEEE Aerospace and Electronic Systems Magazine, 32, 38-45. https://doi.org/10.1109/MAES.2017.160174
DOI
|
22 |
Pachter, M. Welker, T. C., & Huffman, R. E. Jr. 2013, Gyrofree INS theory, Navigation: Journal of The Institute of Navigation, 60, 85-96. https://doi.org/10.1002/navi.32
DOI
|
23 |
Park, C. 1996, Attitude determination from GPS carrier phase measurements, PhD Thesis, Seoul National University.
|
24 |
Park, S. & Tan, C.-W. 2002, GPS-aided gyroscope-free inertial navigation systems, California PATH Research Report, UCB-IRS-PRR-2002-22.
|