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Recent Advances in Electrical & Electronic Engineering

Recent Advances in Electrical & Electronic Engineering

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ISSN (Print): 2352-0965
ISSN (Online): 2352-0973

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Review Article

Development Status and Future Prospects of Strapdown Inertial Navigation Technology

Author(s): Hongbo Liu, Juncheng Wu, Yuze Lin and Xiaodong Yang*

Volume 18, Issue 10, 2025

Published on: 06 January, 2025

Article ID: e23520965347882

Pages: 16

DOI: 10.2174/0123520965347882241024082952

Price: $65

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Abstract

Background: Inertial navigation is a comprehensive technology involving precision machinery, computer technology, microelectronics, optics, automatic control, materials, and other disciplines and fields. Strapdown inertial navigation systems have gradually developed into the mainstream and direction of inertial navigation systems because of their small size, low cost, simple structure, and high reliability. The angular rate and acceleration information of the carrier relative to the inertial space are measured by the inertial measurement unit (IMU), and the instantaneous velocity and position information of the carrier are automatically calculated by Newton's law of motion. It has the characteristics of not relying on external information, not radiating energy to the outside world, not being disturbed, and good concealment. Therefore, it is widely used in aerospace, aviation, and navigation, especially in the military field.

Objective: This paper describes the development history of the Strapdown Inertia Navigation System summarizes the research status of the Strapdown Inertia Navigation System, and looks forward to its future development direction.

Methods: The key technologies of strapdown inertial navigation systems are investigated, and the related research on strapdown inertial navigation technology is understood in detail. The hardware composition and related algorithms of the strapdown inertial navigation system are analyzed in detail.

Results: Nowadays, strapdown inertial navigation technology is the mainstream of inertial navigation technology. Compared with the gimbaled inertial navigation system technology, the strapdown inertial navigation system has higher precision, smaller volume, and lower cost. At present, the initial alignment technology, error compensation technology, navigation algorithm technology, and inertial device technology of strapdown inertial navigation technology have made full development.

Conclusion: With the development of initial alignment technology, error compensation technology, navigation algorithm technology, and inertial device technology, the accuracy, response speed and anti-interference ability of strapdown inertial navigation technology have been significantly improved. The development of strapdown inertial navigation is closely related to the gyroscope technology which belongs to inertial device technology. The strapdown inertial navigation system based on optical gyroscopes such as laser gyroscopes and fibre optic gyroscopes is mature, and the MEMS strapdown inertial navigation system has a wide application prospect compared with the optical gyroscope strapdown inertial navigation system.

Keywords: Strapdown inertial navigation system, gyroscope, initial alignment, error compensation, inertial technology, accelerometer.

Graphical Abstract

Graphical abstract illustrating key findings of the study

[1]
X. Yuan, J.X. Yu, and Z. Chen, Navigation system., Aviation Industry Publishing House: Beijing, 1993.
[2]
B. Chatfield, Averil, fundamentals of high accuracy inertial navigation., American Institute of Aeronautics and Astronautics: Reston, 1997.
[http://dx.doi.org/10.2514/4.866463]
[3]
M.S. Grewal, L.R. Weill, and A.P. Andrews, Global positioning systems, inertial navigation, and integration., John Wiley & Sons, 2007.
[http://dx.doi.org/10.1002/0470099720]
[4]
W. Wang, "Status and Development Trend of Inertial Technology", Zidonghua Xuebao, vol. 39, no. 6, pp. 723-729, 2014.
[http://dx.doi.org/10.3724/SP.J.1004.2013.00723]
[5]
X.C. Zhou, and J.S. Shen, "Development of inertial navigation technology and its applications", Autom. Meas. Control, vol. 25, no. 9, pp. 55-59, 2006.
[6]
H.G. Ding, Inertia technology collection., National Defense Industry Press: Beijing, 1994.
[7]
X.L. Wang, Initial alignment of dynamic and static base of strapdown inertial navigation system., Northwest Industrial University Press, 2013.
[8]
S.C. Garg, L.D. Morrow, and R. Mamen, "Strapdown navigation technology: A literature survey", J. Guid. Control, vol. 1, no. 3, pp. 161-172, 1978.
[http://dx.doi.org/10.2514/3.55760]
[9]
Y.J. Lu, Inertial Device(I&II)., China Astronautic Publishing House: Beijing, 1990.
[10]
Y.Y. Qin, Inertial navigation., Beijing: Science Press, 2014.
[11]
Y.L. Wu, "Application of ocean current velocity estimation in strapdown compass alignment", M.S. thesis, National University of Defense Technology, Changsha, China, 2021.
[12]
J. Bortz, "A new mathematical formulation for strapdown inertial navigation", IEEE Trans. Aerosp. Electron. Syst., vol. AES-7, no. 1, pp. 61-66, 1971.
[http://dx.doi.org/10.1109/TAES.1971.310252]
[13]
R.B. Miller, "A new strapdown attitude algorithm", J. Guid. Control Dyn., vol. 6, no. 4, pp. 287-291, 1983.
[http://dx.doi.org/10.2514/3.19831]
[14]
Y.F. Jiang, and Y.P. Lin, "Improved strapdown coning algorithms", IEEE Trans. Aerosp. Electron. Syst., vol. 28, no. 2, pp. 484-490, 1992.
[http://dx.doi.org/10.1109/7.144574]
[15]
H. Musoff, and J.H. Murphy, "Study of strapdown navigation attitude algorithms", J. Guid. Control Dyn., vol. 18, no. 2, pp. 287-290, 1995.
[http://dx.doi.org/10.2514/3.21382]
[16]
Z.L. Deng, Inertial Navigation Principle., Harbin University of Technology Press: Harbin, 1994.
[17]
D.H. Titterton, and J.L. Weston, Strapdown Inertial Navigation Technology., 2nd ed MIT Lincoln Laboratory: Lexington, 2004.
[http://dx.doi.org/10.1049/PBRA017E]
[18]
N. Barbour, and G. Schmidt, "Inertial sensor technology trends", In Workshop on Autonomous Underwater Vehicles Cambridge, 1998, pp. 55-62.
[19]
X.M. Zhao, J. Weng, W. Huang, and Y.X. Zhao, "Inertial navigation technology and modern economy", In The 14th Branch of the 15th Annual Conference of China Association for Science and Technology: Proceedings of the Forum on Civil-Military Integration Development of National Defense Science and Technology Industry China, 2013.
[20]
M.H. Wang, and W. Liu, "GPS/SINS speed integral matching alignment based on improved adaptive UKF", In 2019 2nd World Conference on Mechanical Engineering and Intelligent Manufacturing (WCMEIM) 2019, pp. 352-357.
[21]
L.G. Chen, J.Y. Liu, Y.R. Sun, and M. Yue, "Study of analytic coarse alignment methods to micro SINS", Hangtian Kongzhi, vol. 23, no. 4, pp. 9-12, 2005.
[22]
C.L. Wei, and H.Y. Zhang, "Comparison of analytic coarse alignment methods", Hangtian Kongzhi, vol. 18, no. 3, pp. 16-21, 2000.
[23]
G.M. Yan, Research on initial alignment of strapdown inertial navigation system on moving base and other related problems., Northwestern Polytechnical University, 2008.
[24]
J. Zhao, "Study of the self-alignment method under latitude unknown in dynamic disturbance condition", M.S. thesis, Beijing: Beijing Polytechnic University, 2016.
[25]
S. Julier, J. Uhlmann, and H.F. Durrant-Whyte, "A new method for the nonlinear transformation of means and covariances in filters and estimators", IEEE Trans. Automat. Contr., vol. 45, no. 3, pp. 477-482, 2000.
[http://dx.doi.org/10.1109/9.847726]
[26]
Z. Zhanxin, G. Yanan, and C. Liabin, "Unscented Kalman filter for SINS alignment", J. Syst. Eng. Electron., vol. 18, no. 2, pp. 327-333, 2007.
[http://dx.doi.org/10.1016/S1004-4132(07)60094-2]
[27]
Guanglong Du, and Ping Zhang, "Online serial manipulator calibration based on multisensory process via extended kalman and particle filters", IEEE Trans. Ind. Electron., vol. 61, no. 12, pp. 6852-6859, 2014.
[http://dx.doi.org/10.1109/TIE.2014.2314051]
[28]
B. Wang, W. Ye, and Y. Liu, "An improved real-time transfer alignment algorithm based on adaptive noise estimation for distributed POS", IEEE Access, vol. 8, pp. 102119-102127, 2020.
[http://dx.doi.org/10.1109/ACCESS.2020.2998719]
[29]
X. Liu, Q.S. Zhang, and D.K. Yang, "Nonlinear filter algorithm for GPS/DR integrated positioning", J. Beijing Uni. Aeronautics and Astronautics, vol. 33, no. 2, pp. 184-187, 2007.
[30]
D.L. Wang, and H.Y. Zhang, "Nonlinear Filtering Algorithm for INS Initial Alignment", Chinese J. Inertial Tech., vol. 7, no. 3, pp. 18-22, 1999.
[31]
D.M. Li, "Study on initial alignment methods of strapdown inertial navigation system", Ph.D. thesis, Harbin Engineering University, Harbin, China, 2006.
[32]
T. Gaiffe, Y. Cottreau, N. Faussot, G. Hardy, P. Simonpietri, and H. Arditty, "Highly Compact fiber optic gyrocompass for applications at depths up to 3,000 meters", In Proceedings of the 2000 International Symposium on Underwater Technology (Cat. No.00EX418) Tokyo, Japan, 26-26 May 2000, pp. 155-160.
[33]
T. Gaiffe, "From R&D brassboard to navigation grade FOG-based INS: The experience of photonetics/lxsea", In 15th Optical Fiber Sensors Conference Technical Digest., 2002 Portland, OR, USA, 10-10 May 2002, pp. 1-4.
[34]
F. Napolitano, T. Gaiffe, Y. Cottreau, and T. Loret, "PHINS: The first high performances inertial navigation system based on fiber optic gyroscopes", In 9th Saint Petersburg International Conference on Integrated Navigation systems, 2002pp. 296-304 Saint Petersburg, Russia, 2002, pp. 1-4.
[35]
Y.Y. Qin, G.M. Yan, and D.Q. Gu, "Study on information-based coarse alignment of strapdown inertial navigation system on swing base", J. Northwestern Polytech. Uni., vol. 23, no. 5, pp. 681-684, 2005.
[36]
X.J. Lian, Y.G. Tang, M.P. Wu, and X.P. Hu, "Study on SINS alignment algorithm with inertial frame for swaying bases", Guofang Ke-ji Daxue Xuebao, vol. 25, no. 5, pp. 95-99, 2007.
[37]
G.M. Yan, W.S. Yan, and D.M. Xu, "Reverse navigation algorithm and its application in initial alignment of strapdown compass base", In Essays of the 27th China Control Conference, China, 2008.
[38]
Q. Zhou, Y.Y. Qin, J.H. Zhang, and Y. Cheng, "Initial alignment algorithm for SINS based on quaternion Kalman filter", Journal of Chinese Inertial Technology, vol. 20, no. 2, pp. 162-167, 2012.
[39]
X. Cui, Y.Y. Qin, G.M. Yan, and Q. Zhou, "Initial alignment algorithm for SINS based on state matrix Kalman filter", J. Chinese Inertial Technol., vol. 26, no. 5, pp. 31-36, 2018.
[40]
C.S. Giovanni, and E. Levinson, "Performance of a ring laser strapdown marine gyrocompass", In ION 37th Annual Meeting Proceedings Maryland, USA, 1981, pp.311-341.
[http://dx.doi.org/10.1002/j.2161-4296.1981.tb00779.x]
[41]
E. Levinson, and R. Majure, "Accuracy enhancement techniques applied to the marine ring laser inertial navigator (MARLIN)", Navigation (Washington), vol. 34, no. 1, pp. 64-86, 1987.
[http://dx.doi.org/10.1002/j.2161-4296.1987.tb01490.x]
[42]
J. DeWall, "Ship Augmented Gravity Enhancement (SAGE)", In Proceedings of IEEE/ION PLANS 2006 San Diego, CA, April 2006, pp. 36-43.
[43]
Y.M. Lu, "Auto compensation of dither RLG INS", Journal of Chinese Inertial Technology, vol. 14, no. 4, pp. 18-21, 2006.
[44]
L.J. Miao, "Research on the application of wavelet analysis in optical fiber tuo tuo signal filtering", J. Astronaut., vol. 21, no. 1, pp. 42-46, 2000.
[45]
W. Tang, S.X. Li, L.Y. Liu, and Y. Yang, "Select of wavelet basis in gyro signal processing", Chinese Journal of Inertia Technology, vol. 10, no. 5, pp. 29-31, 2002.
[46]
Y.N. Gao, and J.B. Chen, "Wavelet analysis in the signal processing of FOG", Fire Power and Control, vol. 30, no. 5, pp. 35-37, 2005.
[47]
R.M. Yuan, X.H. Wei, Z.Y. Li, and R.X. Yuan, "De-noising algorithm for signal in fog based on wavelet filtering using threshold value", Chinese J. Inertia Tech., vol. 11, no. 5, pp. 43-48, 2003.
[48]
W. Guo, P.F. Yang, W.G. Zhang, and W. Wang, "Error compensation method for MEMS accelerometer based on BP neural network model", China Measurement and Test, vol. 44, no. 3, pp. 109-113, 2018.
[49]
C. Zhuo, and J.B. Du, "Thermal error compensation algorithm for accelerometers based on differential measurement of specific force", Chinese J. Inertia Techn., vol. 24, no. 6, pp. 821-827, 2016.
[50]
J.X. Lian, D.W. Hu, X.P. Hu, and W.Q. Wu, "Research on coning error and quantization error of SINS attitude algorithm", Hangkong Xuebao, vol. 27, no. 1, pp. 98-101, 2006.
[51]
X.Y. Wei, "Research on attitude algorithm of strapdown inertial navigation system", M.S. thesis, Harbin Institute of Technology, Harbin, China., 2005.
[52]
H. Lu, and X.F. Wei, "Simulation research and overall design for SINS of air-to-air missile", Electronics Optics &Control, vol. 14, no. 2, pp. 128-132, 2007.
[53]
P.G. Savage, "A unified mathematical framework for strapdown algorithm design", J. Guid. Control Dyn., vol. 29, no. 2, pp. 237-249, 2006.
[http://dx.doi.org/10.2514/1.17112]
[54]
P.G. Savage, "Strapdown inertial navigation integration algorithm design part 1: Attitude algorithms", J. Guid. Control Dyn., vol. 21, no. 1, pp. 19-28, 1998.
[http://dx.doi.org/10.2514/2.4228]
[55]
X.Y. Liu, "The research of SINS velocity algorithm based on the virtual slewing coordinate system", M.S. thesis, Harbin Institute of Technology, Harbin, China, 2016.
[56]
P.G. Savage, "Strapdown inertial navigation integration algorithm design part 2: velocity and position algorithms", J. Guid. Control Dyn., vol. 21, no. 2, pp. 208-221, 1998.
[http://dx.doi.org/10.2514/2.4242]
[57]
H. Xiao, Y.Z. Chen, and H.Y. Yang, "Improved velocity algorithm of SINS based on FOG", J. Projectiles Rockets Missiles Guid., vol. 30, no. 1, pp. 80-83, 2010.
[58]
D.Q. Gu, Y.Y. Qin, J. Li, and J.F. Duan, "Research on multi-sample algorithms for position updating of SINS", Fire Control and Command Control, vol. 31, no. 6, pp. 8-10, 2006.
[59]
M.B. Ignagni, "Optimal strapdown attitude integration algorithms", J. Guid. Control Dyn., vol. 13, no. 2, pp. 363-369, 1990.
[http://dx.doi.org/10.2514/3.20558]
[60]
J.G. Mark, and D.A. Tazartes, "Tuning of coning algorithms to gyro data frequency response characteristics", J. Guid. Control Dyn., vol. 24, no. 4, pp. 641-647, 2001.
[http://dx.doi.org/10.2514/2.4770]
[61]
Yuanxin Wu, Xiaoping Hu, Dewen Hu, Tao Li, and Junxiang Lian, "Strapdown inertial navigation system algorithms based on dual quaternions", IEEE Trans. Aerosp. Electron. Syst., vol. 41, no. 1, pp. 110-132, 2005.
[http://dx.doi.org/10.1109/TAES.2005.1413751]
[62]
Yuanxin Wu, Xiaoping Hu, Meiping Wu, and Dewen Hu, "Strapdown inertial navigation using dual quaternion algebra: Error analysis", IEEE Trans. Aerosp. Electron. Syst., vol. 42, no. 1, pp. 259-266, 2006.
[http://dx.doi.org/10.1109/TAES.2006.1603421]
[63]
K.M. Hays, R.G. Schmidt, W.A. Wilson, J.D. Campbell, D.W. Heckman, and M.P. Gokhale, "A Submarine Navigator for the 21st Century", In IEEE Position Location and Navigation Symposium Palm Springs, CA, USA, 2002, pp. 179-188.
[http://dx.doi.org/10.1109/PLANS.2002.998906]
[64]
S. Vajda, and A. Zorn, "Survey of existing and emerging technologies for strategic submarine navigation", In IEEE Position Location and Navigation Symposium 1998, pp.309-315.
[http://dx.doi.org/10.1109/PLANS.1998.670102]
[65]
W.G. Clautice, ""Submarine navigation", navigation", J. Inst. Navig., vol. 25, no. l, 1978.
[66]
B. McKELVIE, and H. Galt Jr, "The evolution of the ship’s inertial navigation system for the fleet ballistic missile program", Navigation (Washington), vol. 25, no. 3, pp. 310-322, 1978.
[http://dx.doi.org/10.1002/j.2161-4296.1978.tb02260.x]
[67]
R.L. Greenspan, "Inertial navigation technology from 1970-1995", Navigation (Washington), vol. 42, no. 1, pp. 165-185, 1995.
[http://dx.doi.org/10.1002/j.2161-4296.1995.tb02334.x]
[68]
O.L. Elton, and J.P. Moore, "Marine ESG navigation as a capability for the present", Navigation (Washington), vol. 20, no. 2, pp. 126-136, 1973.
[http://dx.doi.org/10.1002/j.2161-4296.1973.tb01161.x]
[69]
P.E. Hall, and P.O. Hanson, "Performance analysis of an electrically suspended gyro navigator (ESGN) for marine applications", In Proceedings of the ION National Marine Meetings Annapolis, Md., October, 1972.
[70]
M.W. Mcmurran, and J.A. Ling, "Development and testing of a precision marine electrostatic gyroscope", In ION National Meeting West Point, the USA, 1972.
[71]
G.Z. Xu, Inertia technical manual., Astronautical Press: Beijing, 1995.
[72]
E. Levinson, and C.S. Giovanni, "Laser gyro potential for long endurance marine navigation", In IEEE PLANS Position Location Navigation Symposium Piscataway, 1980, Vol. 115, pp.115-129.
[73]
"UrsaNav", Available from: http://www.ursanav.com
[74]
D.W. Heckman, and L.M. Baretela, "Improved affordability of high precision submarine inertial navigation by insertion of rapidly developing fiber optic gyro technology", In IEEE Position Location and Navigation Symposium San Diego, CA, USA, 2000, pp. 404-410
[http://dx.doi.org/10.1109/PLANS.2000.838332]
[75]
R.B. Morrow, and D.W. Heckman, "High precision ifog insertion into the strategic submarine navigation system", In IEEE PLANS Position Location and Navigation Symposium Palm Springs, CA, USA, 1998, pp. 332-338.
[http://dx.doi.org/10.1109/PLANS.1998.670128]
[76]
G. Adams, and M. Gokhale, Fiber optic gyro based precision navigation for submarines., AIAA Guidance, Navigation, and Control Conference and Exhibit: Denver, United States, 2000, pp. 2-6.
[http://dx.doi.org/10.2514/6.2000-4384]
[77]
H.Y. Quan, S.H. Yang, X.Z. Chen, and H. Wang, "Development and application of advanced MEMS solid wave gyroscope", Navigation and Control, vol. 16, no. 6, pp. 74-82, 2013.
[78]
X.Y. Li, W.K. Wang, S.L. Wang, Y.Q. Peng, and X.F. Jin, "Status and development trend of MEMS inertial sensors", Journal of Telemetry, Tracking and Command, vol. 40, no. 6, pp. 1-13, 2019.
[79]
L.L. Xue, Y.P. Shen, and Y. Xu, "Development and review of foreign inertial technology in 2019", Navigation Positioning & Timing, vol. 7, no. 1, pp. 60-66, 2020.
[80]
H.L. Deng, "Overview of quartz vibrating beam accelerometer", Control Technology of Tactical Missile, vol. 21, no. 4, pp. 52-57, 2004.
[81]
"The VIA vibrating beam accelerometer: Concept and performance", In: Proceedings of the 1998 Position Location and Navigation Symposium Palm Springs, CA: IEEE, 1998, pp. 25-29.
[82]
A. Killen, D. Tarrant, and D. Jensen, "High acceleration, high performance solid state accelerometer development", IEEE Aerosp. Electron. Syst. Mag., vol. 9, no. 9, pp. 20-25, 1994.
[http://dx.doi.org/10.1109/62.312975]
[83]
R. Hopkins, J. Miola, W. Sawyer, R. Setterlund, and B. Dow, "The Silicon oscillating accelerometer: A high-performance MEMS accelerometer for precision navigation and strategic guidance application", In Proceedings of the 61st Annual Meeting of the Institute of Navigation Cambridge, MA, 2005, pp. 1043-1052.
[84]
Y.Q. Liu, S.Z. Wang, and H. Li, "Damping technology in strapdown inertial navigation system", Aerodynamic Missile, no. 8, pp. 44-60, 1990.
[85]
J.J. Yao, "Contrast of different vibration isolation patterns used in strapdown inertial navigation system", Structure & Environment Engineering, vol. 36, no. 2, pp. 19-27, 2009.
[86]
Z.H. Tuo, D.W. Hu, R.H. Li, and J.C. Wei, "Damping design of strapdown inertial navigation system", J Chinese Inertial Technol., vol. 17, no. 6, pp. 648-650, 2009.
[87]
Z.Q. Yao, H.J. Lei, H.W. Song, and Y. Zhang, "Fine modeling for coupled vibration problem of laser strap-down inertial navigation", Journal of Vibration and Shock, vol. 38, no. 21, pp. 271-277, 2019.
[88]
X.B. Li, B. Wu, C. Dong, and B.L. Li, "Research on coupled vibration of strapdown INS damping system", Equipment Environmental Engineering, vol. 11, no. 2, pp. 43-49, 2014.
[89]
B. Zhang, and J. Ren, "Coupling vibration analysis of spatial-five-point arrangement isolators for strapdown inertial navigation system", J. Astronaut., vol. 36, no. 9, pp. 1030-1035, 2015.
[90]
Z.X. Zhang, and D.W. Zhang, "Theory analysis on resonance frequencies of linear vibration and torsional vibration of strapdown IMU damping system", J. Chinese Inertial Technol., vol. 17, no. 6, pp. 654-657, 2009.
[91]
X. Zhao, W. Wei, and J. Zhang, "Thedynamic modeling and the structure design method based on the dynamic characteristics of DRLG INS", Navigation and Control, vol. 19, no. 6, pp. 35-43, 2020.
[92]
L. Luo, Y.L. Huang, L.B. Chang, and Y.G. Zhang, "Development and prospects of initial alignment method for strap-down inertial navigation system", Chinese J. Ship Res., vol. 17, no. 5, pp. 301-313, 2022.
[93]
X. Yuan, and E. Zheng, Strapdown Inertial Navigation Principle., Aviation Professional Textbook Compilation Group: Nanjing, 1985.
[94]
Jiang Hong, Yang Wei-Qin, and Yang You-Tang, "State space modeling of random drift rate in high-precision gyro", IEEE Trans. Aerosp. Electron. Syst., vol. 32, no. 3, pp. 1138-1143, 1996.
[http://dx.doi.org/10.1109/7.532273]
[95]
Y.R. Lin, and Z.L. Deng, "Systematic calibration for inertial instruments errors in laser gyro strapdown iinertial navigation system", J. Harbin Inst. Technol., vol. 33, no. 1, pp. 112-115, 2001.
[96]
M.F. Guo, Y.H. Teng, and Y.S. Zhang, "Research on the static calibration method for a laser inertial navigation system", Journal of Chinese Inertial Technology, vol. 5, no. 4, pp. 24-27, 1997.
[97]
G.T. Liang, J.J. Hui, and Y.P. Li, "Development and application of gyroscope", Aerodynamic Missile J., no. 4, pp. 38-40, 2006.
[98]
J.H. Chen, "Gyroscope and inertial navigation", physics, vol. 24, no. 6, pp. 348-354, 1995.
[99]
F. Aronowitz, "The Laser Gyro", In: M. Ross, Ed., Laser Applications New York., Academic Press, 1971.
[100]
W.W. Chow, J. Gea-Banacloche, L.M. Pedrotti, V.E. Sanders, W. Schleich, and M.O. Scully, "The ring laser gyro", Rev. Mod. Phys., vol. 57, no. 1, pp. 61-104, 1985.
[http://dx.doi.org/10.1103/RevModPhys.57.61]
[101]
J.R. Wilkinson, "Ring lasers", Prog. Quantum Electron., vol. 11, no. 1, pp. 1-103, 1987.
[http://dx.doi.org/10.1016/0079-6727(87)90003-6]
[102]
M. Faucheux, D. Fayoux, and J.L. Roland, "The ring laser gyro", Journal of Optics(Paris), vol. 19, no. 3, pp. 101-115, 1988.
[103]
X.D. Yu, "Research on some key technologies for single-axis rotation inertial navigation system with mechanically dithered ring laser gyroscope", M.S. thesis, National University of Defense Technology, Changsha, China., 2011.
[104]
Y. Liu, "The research on the shipboard strapdown vertical reference unit based on fiber optic gyroscope", M.S. thesis, Harbin Institute of Technology, Harbin, China., 2011.
[105]
S.H. Wang, "Current status and applications of MEMS sensors", Weina Dianzi Jishu: Micronanoelectronic Technology, vol. 48, no. 8, pp. 516-522, 2011.
[106]
H. Wang, "MEMS gyroscope sensor ASIC Introduction and design", China lntegrated Circult., vol. 28, no. 6, pp. 44-50, 2019.
[107]
H.F. Liu, S.M. Jiao, and L.C. Tu, "Status and trend of optomechanical accelerometers abroad", Navigation and Control, vol. 20, no. 3, pp. 1-8, 2021.
[108]
W. Wang, "The analysis and design of high-precision accelerometer measurement system", M.S. thesis, Harbin Engineering University, Harbin, China., 2011.

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