An Overview of the Current Research Status of Gyro-Free Inertial Measurement Technology

Authors

  • Yong Li
  • Fei Shang

DOI:

https://doi.org/10.6919/ICJE.202502_11(2).0001

Keywords:

Gyro-Free Inertial Measurement; Accelerometer Configuration; Angular Velocity.

Abstract

Gyro-free inertial measurement technology utilizes an array of accelerometers to replace traditional gyroscopes for measuring the attitude of a carrier. By synthesizing existing literature, this paper summarizes the research on gyro-free strapdown inertial measurement technology. It conducts comparative analysis on two aspects: different accelerometer configurations and algorithms for calculating angular velocity. The advantages and disadvantages of corresponding configurations and solution methods are summarized. Finally, future research directions are discussed.

Downloads

Download data is not yet available.

References

[1] Corey Victor B. Measuring angular acceleration with linear acceleration[J]. Control Engineering, 1962, 3(3): 79-80.

[2] Schuler A R, Grammatikos A, Fegley K A. Measuring rotational motion with linear accelerometers[J]. IEEE transactions on aerospace and electronic systems, 1967 (3): 465-472.

[3] Algrain M C. Accelerometer-based platform stabilization[C]//Acquisition, Tracking, and Pointing V. SPIE, 1991, 1482: 367-382.

[4] Chen J H, Lee S C, DeBra D B. Gyroscope free strapdown inertial measurement unit by six linear accelerometers[J]. Journal of Guidance, Control, and Dynamics, 1994, 17(2): 286-290.

[5] Tan C W, Park S, Mostov K, et al. Design of gyroscope-free navigation systems[C]//ITSC 2001. 2001 IEEE Intelligent Transportation Systems. Proceedings (Cat. No. 01TH8585). IEEE, 2001: 286-291.

[6] Lee S C, Huang Y C. Innovative estimation method with measurement likelihood for all-accelerometer type inertial navigation system[J]. IEEE transactions on Aerospace and Electronic Systems, 2002, 38(1): 339-346.

[7] Tsai Y L, Tu T T, Bae H, et al. EcoIMU: A dual triaxial-accelerometer inertial measurement unit for wearable applications[C]//2010 International Conference on Body Sensor Networks. IEEE, 2010: 207-212.

[8] SHI Zhen Accelerometer Allocation Scheme in Gyroscope Free Strapdown Inertial Navigation System[J]. Journal of Chinese Inertial Technology, 2002(01): 16-20.

[9] Padgaonkar A J, Krieger K W, King A I. Measurement of angular acceleration of a rigid body using linear accelerometers[J]. 1975.

[10] Ma Shutian,Chen Shiyou, Li Yanmei, Zhang Haixia NONGYROSCOPIC STRAPDOWN INERTIAL NAVIGATION SYSTEM[J]. ACTA AERONAUTICA ET ASTRONAUTICA SINICA, 1997(04): 101-105.

[11] WANG Jin song,WANG Qi, SUN ShengheGyros-free inertial measurement unit[J]. Journal of Transducer Technology, 2003(04): 43-45.

[12] XiaoWeiguang, DU Zuliang, WANG QiA Practical Design of a Nine-accelerometer NGMIMU[J]. Journal of Astronautics, 2006(03): 478-482.

[13] Buhmann A, Peters C, Cornils M, et al. A GPS aided full linear accelerometer based gyroscope-free navigation system[C]//Proceedings of IEEE/ION PLANS 2006. 2006: 622-629.

[14] Parsa K, Lasky T A, Ravani B. Design and implementation of a mechatronic, all-accelerometer inertial measurement unit[J]. IEEE/ASME Transactions on Mechatronics, 2007, 12(6): 640-650.

[15] WANG Xiaona, WANG Shuzong, ZHU Huabing. Study on Models of Gyroscope-free Strap-down Inertial Navigation System[J]. Acta Armamentarii, 2006(02): 288-292.

[16] Mu Shuzhi Simulation and Experiment of Nongyroscopic Inertial Measurement Unit[D]. Chinese Doctoral Dissertations Full-text Database, 2007.

[17] ZHANG Huixin,WANG Shichang, YANG Yunliang. Method optimization for angular velocity calculating in inertial testing system composed with full accelerometers[J]. Journal of Chinese Inertial Technology, 2008, 16(06): 672-675.

[18] Cai Guowen. Rotating Projectile Attitude Measurement Based on Full Accelerometers[D]. Chinese Master's Theses Full-text Database, 2018.

[19] Yang Jie. Accelerometer Configuration and Error Analysis for GFSINS[D]. Chinese Doctoral Dissertations Full-text Database, 2011.

[20] Liu Zhiping. Research on Several Key Technologies of GFSINS[D]. Chinese Doctoral Dissertations Full-text Database, 2010.

[21] XiongYonghu,MA Baohua. The Nongyroscope Strap down Inertial Navigation Method for Trajectory Correcting Fuzes[J]. JOURNAL OF DETECTION & CONTROL, 1999(04): 3-6.

[22] Orlando V, Neto A R, Kuga H K. Batch and sequential data smoothing and compression by curve fitting using and adaptive state estimation technique[J]. 1986.

[23] Ma Shutian. Research on Strapdown Inertial Navigation System without Gyroscopes [R]. Beijing: China Shipbuilding Industry Corporation.

[24] Zhao Jianwei, Ma Shutian. Methods to Improve Angular Velocity Calculation Accuracy in Strapdown Inertial Navigation Systems without Gyroscopes [J]. Automation Technology and Application in Heilongjiang, 1999, (05): 42-44.

[25] Zhao Long, CHEN Zhe. A New Method for Improving the Angular Velocity Calculation Precision of Gyroscope-Free Strapdown Inertial Navigation System[J]. Acta SimulataSystematica Sinica, 2003(04): 579-580+603.

[26] CaoYonghong, Zhang Hui, FAN Jinbiao. Research on Attitude Optimization Algorithm of Projectile at All Accelerometers' Installation Errors Based on GFIMU[J]. Acta Armamentarii, 2009, 30(02): 170-174.

[27] Ding Mingli, Wang Qi, Hong liang. A Kalman-filtering Approach for a Non-gyro Micro Inertial Measurement Unit[J]. Chinese Journal of Scientific Instrument, 2003(S1): 310-313.

[28] WangWei,DaiYingjie,ChenHailong, et al. Application of Kalman filter to calculate angular velocity of complicated vibration by full acceleration sensor[J]. China Measurement & Test, 2017, 43(05): 105-109+119.

[29] Chen Yang,Yang Di, Cui Hutao. GYROLESS ATTITUDE AND RATE ESTIMATION USING SINGER MODEL[J]. Acta Aeronautica Et Astronautica Sinica, 2002(06): 507-511.

[30] ZhaoGuorong,ChenMuqing. Attitude Angular Velocity Algorithm for Nine-Accelerometer GFSINS[J]. Journal of System Simulation, 2007(14): 3350-3353.

[31] Zhao Xia. The Application of the Extended Kalman Filer Algorithm to the Angular Velocity Calculation of GFSINS[J]. Journal of Projectiles,Rockets,Missiles and Guidance, 2008(04): 52-54.

[32] Liu Tao, Zhao Guorong, Li Jixin. Application of H∞ Filtering in Strapdown Inertial Navigation Systems without Gyroscopes [J]. Journal of Chinese Society of Inertial Technology, 2009, 17(1): 28-32.

[33] WangJinsong,Wang Qi SunShenghe. Optimum Technology of GFMIMU[J]. Journal of Nanjing University of Science and Technology, 2004(01): 24-28.

[34] Liu Chaojun. Research on Key Techniques of Gyro-Free Inertial Measurement Units[D]. Chinese Doctoral Dissertations Full-text Database, 2016.

Downloads

Published

2025-01-17

Issue

Section

Articles

How to Cite

Li, Yong, and Fei Shang. 2025. “An Overview of the Current Research Status of Gyro-Free Inertial Measurement Technology”. International Core Journal of Engineering 11 (2): 1-9. https://doi.org/10.6919/ICJE.202502_11(2).0001.