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Journal articles on the topic 'Strap-Down'

Author: Grafiati

Published: 2 June 2025

Last updated: 31 July 2025

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1

Kunken, Frederic R., Ellen M. McGee, and Lance K. Stell. "Case Study: Strap Him down." Hastings Center Report 31, no. 1 (2001): 24. http://dx.doi.org/10.2307/3528729.

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2

Gao, Wei, Benbing Gao, Hongsong Fang, and Xin Lu. "Estimation of Full Strap-down Rotating Bomb Guidance Information Based on Unscented Kalman Filter." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 3 (2020): 604–9. http://dx.doi.org/10.1051/jnwpu/20203830604.

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In this paper, the full strap-down seeker of rotating bomb is taken as the research object, and the method of extracting the LOS (line-of-sight) angle and angular rate of the full strap-down seeker of the rotating bomb is studied. The structure of the full strap-down seeker is quite different from that of the conventional rate gyro seeker. The measurement system of full strap-down seeker is fixed to the missile, the seeker can only obtain the measurement information in the projectile coordinate system, and the measurement information is coupled with the body posture information, so it cannot b

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3

Li, Jun, Shifeng Zhang, and Zhenlin Ma. "Improving the Orbit Injection Accuracy of a Launch Vehicle by Using a Mode-Switching Strategy for a Dual-Axis Rotational Inertial Navigation System." Sensors 25, no. 1 (2024): 177. https://doi.org/10.3390/s25010177.

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Due to a short flight time, the dual-axis rotational inertial navigation system carried by some launch vehicles or missiles is often only used for self-calibration and self-alignment. It is generally in the strap-down state rather than the rotation modulation state during flight. This wastes the precision potential of the navigation system. Therefore, a mode-switching strategy is proposed in this paper to improve the orbit injection accuracy of a launch vehicle. The rotational navigation system of the launch vehicle is in the near-platform mode or strap-down mode at different periods. It is sw

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4

WANG Yong-wei, 王永伟, 徐向东 XU Xiang-dong, 高峰 GAO Feng, 穆岩 MU Yan, and 宫亚坤 GONG Ya-kun. "Signal sampling system of strap-down north seeking." Chinese Journal of Optics and Applied Optics 7, no. 5 (2014): 786–93. http://dx.doi.org/10.3788/co.20140705.0786.

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5

Sheng, Hanlin, and Tianhong Zhang. "MEMS-based low-cost strap-down AHRS research." Measurement 59 (January 2015): 63–72. http://dx.doi.org/10.1016/j.measurement.2014.09.041.

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6

Nguyen Trong Khuyen. "Researching and building a method for testing and adjusting the strapdown inertial navigation system." Journal of Military Science and Technology, CSCE5 (December 15, 2021): 24–31. http://dx.doi.org/10.54939/1859-1043.j.mst.csce5.2021.24-31.

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The strap-down inertial navigation system (SINS) is widely used and becoming very important in many areas, especially in the arms industry when the GPS signal is lost or not reliable. To ensure the precision of the system, in addition to optimizing the algorithm for the strap-down inertial navigation system, the testing, and adjusting of the SINS system when installed on vehicles also play a vital role. In the article, a method of displaying SINS data on a digital map is proposed. Furthermore, the article also proposes a method to assess the influence of misalignment angles on the navigation a

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7

An, Xiao Xue, Xiao Dong Chai, Wen Fa Zhu, and Xiao Wei Xu. "Software Design of the Track State Inspection System Based on LabVIEW." Advanced Materials Research 546-547 (July 2012): 1323–28. http://dx.doi.org/10.4028/www.scientific.net/amr.546-547.1323.

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This paper describes the software of the track state inspection system based on LABVIEW, which includes serial communication, data extraction, strap-down algorithm, acceleration integral and saving the results. Serial communication module uses VISA to program in order to realize communication between the IMU (inertial measurement unit)and upper computer. According to the output data format, data extraction module separates the signal of three axes’ accelerations and angular-rates by Match Pattern Function. Strap-down algorithm and acceleration integral modules are programmed by Math Script. Th

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8

Wang Wei, 王. 伟., 纪. 毅. Ji Yi, 石忠佼 Shi Zhongjiao, 林德福 Lin Defu, and 林时尧 Lin Shiyao. "EKF-based scaling factor identification for strap-down seeker." Infrared and Laser Engineering 46, no. 4 (2017): 417003. http://dx.doi.org/10.3788/irla201746.0417003.

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9

Zhang, Xi, Jie Li, Li Qin, and Chong Shen. "Comprehensive Calibration of Strap-Down Tri-Axis Accelerometer Unit." Micromachines 8, no. 3 (2017): 68. http://dx.doi.org/10.3390/mi8030068.

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10

Wang, Yawei, Weihu Zhou, Xiaoquan Han, Zhongyu Wang, and Jinbin Ding. "Strap‐down stabilization for multi‐load optoelectronic imaging platform." Aircraft Engineering and Aerospace Technology 84, no. 2 (2012): 94–102. http://dx.doi.org/10.1108/00022661211207901.

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11

Fugui, Li, Jia Shengwei, Tong Zeyou, et al. "Guidance and Control Method for Vehicle with Strap-down Seeker." MATEC Web of Conferences 291 (2019): 01003. http://dx.doi.org/10.1051/matecconf/201929101003.

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Guidance and control method was presented in this paper for flight vehicle with a strap-down seeker. Firstly, an extended Kalman filter was constructed in LOS (line of sight) coordinate system to estimate the guidance signal based on the information measured by strap-down seeker and inertial measurement unit. Secondly, an optimal guidance law which could reduce the target maneuvering and guidance system dynamics was proposed. Thirdly, three-loop acceleration autopilot with pseudo-angle of attack feedback was presented to control the flight vehicle. Finally, the proposed methods were simulated

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12

Zhu, Lu Feng, and Chun Xi Zhang. "The Fine System-Level Calibration Technique of Size Effect Error for the Fiber-SINS." Advanced Materials Research 383-390 (November 2011): 2060–65. http://dx.doi.org/10.4028/www.scientific.net/amr.383-390.2060.

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A fine system-level calibration technique of size effect error is presented for Fiber-strap-down inertial navigation systems (Fiber-SINS) in this paper. When the strap-down system is mounted onto high precision turntable and rotating along predefined trajectory, the velocity errors can contain information related to the size effect error, which can be estimated accurately by Kalman filter. In this paper, principles of the calibration technique are emphasized, the model of the size effect error is presented and Hardware-in-the-Loop Simulation platform is designed to validate the efficiency of t

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13

Li, Jian Rong, Cheng Wu Shen, and Shao Jin Liu. "Research on High Precision Temperature Control System of Strap-Down North-Seeking." Applied Mechanics and Materials 740 (March 2015): 269–73. http://dx.doi.org/10.4028/www.scientific.net/amm.740.269.

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In order to make the dynamically tuned gyroscope of Strap-down North-seeking working on the best temperature environment, reduce errors caused by temperature changes, a high-precision temperature control system is built up on the base of control theory and engineering. This system is a two-stage temperature control system. In order to realize high precision temperature control at a predetermined temperature range, temperature measurement circuit is analyzed and calculated on a two-stage temperature control had different measurement circuit match. Experimental results show that the accuracy of

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14

Tamer, Mekky Ahmed. "Necessary Modifications to the Strap-Down Inertial Navigation System Model for Non-Earth-Based Users." International Journal of Aeronautical Science & Aerospace Research 1, no. 2 (2014): 11–20. https://doi.org/10.19070/2470-4415-140002.

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Strap-down inertial navigation system (SDINS) is considered as a highly sophisticated dead reckoning system. The SDINS consists mainly of two triads the first is the three gyros triad, and the second is the three accelerometers triad. Modeling the SDINS has achieved a lot of importance in the literature, especially for surveying applications. However, using the SDINS for spacecraft applications imply some modifications to the SDINS deterministic models used for surveying applications. Traditional models of the SDINS include the effect of the earth rotational rate on the SDI

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15

Grigorie, Lucian T., and Ruxandra M. Botez. "MODELING AND NUMERICAL SIMULATION OF AN ALGORITHM FOR THE INERTIAL SENSORS ERRORS REDUCTION AND FOR THE INCREASE OF THE STRAP-DOWN NAVIGATOR REDUNDANCY DEGREE IN A LOW COST ARCHITECTURE." Transactions of the Canadian Society for Mechanical Engineering 34, no. 1 (2010): 1–16. http://dx.doi.org/10.1139/tcsme-2010-0001.

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In this paper, an algorithm for the inertial sensors errors reduction in a strap-down inertial navigation system, using several miniaturized inertial sensors for each axis of the vehicle frame, is conceived. The algorithm is based on the idea of the maximum ratio-combined telecommunications method. We consider that it would be much more advantageous to set a high number of miniaturized sensors on each input axis of the strap-down inertial system instead of a single one, more accurate but expensive and with larger dimensions. Moreover, a redundant system, which would isolate any of the sensors

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16

Bielenberg, Bob W., Ronald K. Faller, John D. Reid, John R. Rohde, and Dean L. Sicking. "Design and Testing of Tie-Down Systems for Temporary Barriers." Transportation Research Record: Journal of the Transportation Research Board 1851, no. 1 (2003): 83–94. http://dx.doi.org/10.3141/1851-09.

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Two tie-down temporary barrier systems were developed and crash tested according to the safety performance criteria provided in NCHRP Report 350: Recommended Procedures for the Safety Performance Evaluation of Highway Features. Both tie-down systems were designed to reduce barrier displacements and to retain deflected barriers on the bridge deck edge. The first system consisted of a steel tie-down strap concept for use with the Iowa F-shape temporary concrete barrier. At each barrier joint, the trapezoidal-shaped strap retained the vertical pin and was attached to the concrete bridge deck usin

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17

Ibrahim, M. A., and V. V. Luk'yanov. "Algorithms and Configuration for a Moving Object Attitude Control System Based on Microelectromechanical Sensors." Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, no. 2 (131) (June 2020): 44–58. http://dx.doi.org/10.18698/0236-3933-2020-2-44-58.

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Inertial systems for attitude control, stabilisation and navigation of moving objects boast a range of unique qualities, the most important of which are autonomy and interference immunity. At present, strap-down inertial navigation systems using inexpensive and compact microelectromechanical sensors are popular. The biggest disadvantage of the attitude control systems utilising microelectromechanical sensors is rapid error accumulation over time. The main error sources in strap-down inertial navigation systems are the errors of angular velocity sensors and accelerometers. Currently the accurac

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18

Dickson, Peter M., and Philip J. Rae. "The Application of Quaternions to Strap-Down MEMS Sensor Data." Sensors 21, no. 22 (2021): 7658. http://dx.doi.org/10.3390/s21227658.

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We describe the mathematical transformations required to convert the data recorded using typical 6-axis microelectromechanical systems (MEMS) sensor packages (3-axis rate gyroscopes and 3-axis accelerometers) when attached to an object undergoing a short duration loading event, such as blast loading, where inertial data alone are sufficient to track the object motion. By using the quaternion description, the complex object rotations and displacements that typically occur are translated into the more convenient earth frame of reference. An illustrative example is presented where a large and hea

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19

Ghanbarpourasl, Habib. "Attitude reconstruction from strap-down rate gyros using power series." Journal of Navigation 74, no. 4 (2021): 763–81. http://dx.doi.org/10.1017/s0373463321000023.

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AbstractThis paper introduces a power series based method for attitude reconstruction from triad orthogonal strap-down gyros. The method is implemented and validated using quaternions and direction cosine matrix in single and double precision implementation forms. It is supposed that data from gyros are sampled with high frequency and a fitted polynomial is used for an analytical description of the angular velocity vector. The method is compared with the well-known Taylor series approach, and the stability of the coefficients’ norm in higher-order terms for both methods is analysed. It is show

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20

Brown, T. G., B. Davis, D. Hepner, et al. "Strap-down microelectromechanical (MEMS) sensors for high-g munition applications." IEEE Transactions on Magnetics 37, no. 1 (2001): 336–42. http://dx.doi.org/10.1109/20.911850.

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21

Du, Xiao, and Qunli Xia. "Research on strap-down seeker guidance information for rolling interceptor." Optik 129 (January 2017): 183–99. http://dx.doi.org/10.1016/j.ijleo.2016.10.042.

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22

Zhao, Bin, Zhenxin Feng, and Jianguo Guo. "Integral barrier Lyapunov functions-based integrated guidance and control design for strap-down missile with field-of-view constraint." Transactions of the Institute of Measurement and Control 43, no. 6 (2021): 1464–77. http://dx.doi.org/10.1177/0142331220981329.

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The problem of the integrated guidance and control (IGC) design for strap-down missile with the field-of-view (FOV) constraint is solved by using the integral barrier Lyapunov function (iBLF) and the sliding mode control theory. Firstly, the nonlinear and uncertainty state equation with non-strict feedback form for IGC design is derived by using the strap-down decoupling strategy. Secondly, a novel adaptive finite time disturbance observer is proposed to estimate the uncertainties based on an improved adaptive gain super twisting algorithm. Thirdly, the special time-varying sliding variable is

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23

Guo, Jing, Jun Zhou, and Bin Zhao. "Three-dimensional integrated guidance and control for strap-down missiles considering seeker’s field-of-view angle constraint." Transactions of the Institute of Measurement and Control 42, no. 6 (2019): 1097–109. http://dx.doi.org/10.1177/0142331219883719.

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This paper investigates a novel three-dimensional (3D) integrated guidance and control (IGC) method for skid-to-turn (STT) missiles with strap-down seeker. Firstly, a nonlinear IGC model considering seeker’s field-of-view (FOV) constraint is built by employing the strap-down decoupling model, based on which the strict feedback state equation with matched and unmatched uncertainties is derived. Secondly, to handle the FOV angle and the roll angle constraints, an IGC law is proposed by combining dynamic surface control (DSC) approach with integral barrier Lyapunov function (iBLF), by which an ad

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24

Li, Jie, Rui Ping Tao, Jun Liu, and Wei Chen. "Dynamic Research and Design on SINS Damping System in Vehicle." Advanced Materials Research 328-330 (September 2011): 1679–83. http://dx.doi.org/10.4028/www.scientific.net/amr.328-330.1679.

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For the vibration noise problem of strap-down inertial navigation system in the vehicle, a better vibration damping system was designed. Based on the vibration characters of the vehicle environment, a vibration damping model fitted the SINS in the vehicle was presented; and then the mechanism of vibration damping system was designed especially; and then the design of vibration damping system was verified by using of the dynamic characteristic analysis, On the basis of the above analysis, the overall structure of actual vibration isolation system was built, and then the test for the vibration i

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25

Chen, Qiding, Yanwei Luo, and Yan Wang. "Research on line-of-sight angular rate extraction method for strapdown seeker based on AUKF." Journal of Physics: Conference Series 3026, no. 1 (2025): 012060. https://doi.org/10.1088/1742-6596/3026/1/012060.

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Abstract To address the issue that full strap-down seekers cannot directly obtain angular information such as line-of-sight (LOS) angular rates, this study investigates the application of the Adaptive Unscented Kalman Filter algorithm in estimating guidance information. First, the working principles of the fully strap-down seeker and the technical challenges in extracting LOS angles are analyzed. Decoupling formulas for LOS angular rates are derived. The system’s state and observation equations are constructed. Then, considering the non-Gaussian distribution of system measurement noise and the

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26

Li, Jie, Cheng Ye Fan, and Jun Liu. "Algorithm Design of Micro Inertial Strap-Down Heading and Attitude System." Applied Mechanics and Materials 253-255 (December 2012): 1384–87. http://dx.doi.org/10.4028/www.scientific.net/amm.253-255.1384.

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The base theory of micro-inertial strapdown head and attitude systems is expatiate on, and the calculating processes about the strapdown attitude matrix and the body head and attitude angle were discussed thoroughly，at the same time the method of refreshing strapdown matrix by using the quaternion was introduced emphatically. Finally, the result and its analysis about the simulation experiment are given, and the correctness and the validity are proved, some references for our researchers in this field are provided.

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27

Qilong, Xue, Wang Ruihe, Sun Feng, Huang Leilei, and Han Laiju. "Continuous Measurement-While-Drilling Utilizing Strap-Down Multi-Model Surveying System." IEEE Transactions on Instrumentation and Measurement 63, no. 3 (2014): 650–57. http://dx.doi.org/10.1109/tim.2013.2282412.

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28

Thanou, Evangelia, Frank Koopmans, Débora Pita-Illobre, et al. "Suspension TRAPping Filter (sTRAP) Sample Preparation for Quantitative Proteomics in the Low µg Input Range Using a Plasmid DNA Micro-Spin Column: Analysis of the Hippocampus from the 5xFAD Alzheimer’s Disease Mouse Model." Cells 12, no. 9 (2023): 1242. http://dx.doi.org/10.3390/cells12091242.

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Suspension TRAPping filter (sTRAP) is an attractive sample preparation method for proteomics studies. The sTRAP protocol uses 5% SDS that maximizes protein solubilization. Proteins are trapped on a borosilicate glass membrane filter, where SDS is subsequently removed from the filter. After trypsin digestion, peptides are analyzed directly by LC-MS. Here, we demonstrated the use of a low-cost plasmid DNA micro-spin column for the sTRAP sample preparation of a dilution series of a synapse-enriched sample with a range of 10–0.3 µg. With 120 ng tryptic peptides loaded onto the Evosep LC system cou

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29

Zhao, Hong Shan, and Kun Zhang. "Field Test of Automated Strap-Down Vertical Drilling System in Well Anshun-1." Applied Mechanics and Materials 543-547 (March 2014): 387–90. http://dx.doi.org/10.4028/www.scientific.net/amm.543-547.387.

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Automated strap-down vertical drilling system (AVDS) with independent intellectual property rights is composed of a strap-down stabilization platform and a deviation control and correction mechanism. It performs deviation control and correction initiatively while drilling by applying dynamic push-lean, which can effectively solve the inclination control and fast drilling problems arising from high-steep structures and high dip formations. The system can release drilling pressure completely, so under the precondition of ensuring inclination precision, it could remarkably improve the penetration

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30

Elhalwagy, Y., I. Arafa, and Ahmed Youssef. "STRAP DOWN INS ALIGNMENT USING NON-LINEAR MODEL FOR LARGE AZIMUTH MISALIGNMENT." International Conference on Electrical Engineering 5, no. 5 (2006): 1–12. http://dx.doi.org/10.21608/iceeng.2006.33642.

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31

Arafa, Ibrahim, and Ahmed Mohsen. "Strap down INS Alignment Using Non-Linear Model for Large Azimuth Misalignment." International Conference on Electrical Engineering 8, no. 8th (2012): 1–14. http://dx.doi.org/10.21608/iceeng.2012.30666.

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32

JULA, NICOLAE. "AUTONOMOUS AERIAL SURVEILLANCE SYSTEM MOVEMENT MONITORING BY USING STRAP-DOWN INERTIAL TECHNIQUES." Scientific Bulletin of Naval Academy 19, no. 1 (2016): 226–34. http://dx.doi.org/10.21279/1454-864x-16-i1-040.

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33

Egbert, Joseph, and Randal W. Beard. "Low-altitude road following using strap-down cameras on miniature air vehicles." Mechatronics 21, no. 5 (2011): 831–43. http://dx.doi.org/10.1016/j.mechatronics.2010.10.008.

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34

Deng, Zilong, Dongxiao Yang, Xiaohu Zhang, Yuguang Dong, Chengbo Liu, and Qiang Shen. "Real-Time Image Stabilization Method Based on Optical Flow and Binary Point Feature Matching." Electronics 9, no. 1 (2020): 198. http://dx.doi.org/10.3390/electronics9010198.

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The strap-down missile-borne image guidance system can be easily affected by the unwanted jitters of the motion of the camera, and the subsequent recognition and tracking functions are also influenced, thus severely affecting the navigation accuracy of the image guidance system. So, a real-time image stabilization technology is needed to help improve the image quality of the image guidance system. To satisfy the real-time and accuracy requirements of image stabilization in the strap-down missile-borne image guidance system, an image stabilization method based on optical flow and image matching

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35

Liu, Yan Ling, and Xin Zhang. "Simulaion on Strap-Down Inertial Navigation System Based on Simulink/M Programming Language." Applied Mechanics and Materials 467 (December 2013): 584–89. http://dx.doi.org/10.4028/www.scientific.net/amm.467.584.

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This paper presents the basic principles and algorithms of the trap-down Inertial Navigation System, and established the mathematical model and the simulation algorithm of the Inertial Navigation System based on Matlab /Simulink blocks combined with M Programming Language. After the simulation of the system, combined the calculated data, obtained the data error. The result proved that the model is correct and effective.

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36

Elhalwagy, Y., I. Arafa, and K. Mostafa. "COMPUTATIONAL ERRORS OF ANALYTIC COARSE ALIGNMENT FOR STRAP DOWN INERTIAL NAVIGATION SYSTEM (SDINS)." International Conference on Electrical Engineering 5, no. 5 (2006): 1–10. http://dx.doi.org/10.21608/iceeng.2006.33640.

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37

Long, Dafeng, Xiaoming Zhang, Xiaohui Wei, Zhongliang Luo, and Jianzhong Cao. "A Fast Calibration and Compensation Method for Magnetometers in Strap-Down Spinning Projectiles." Sensors 18, no. 12 (2018): 4157. http://dx.doi.org/10.3390/s18124157.

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Attitude measurement is an essential technology in projectile trajectory correction. Magnetometers have been used for projectile attitude measurement systems as they are small in size, lightweight, and low cost. However, magnetometers are seriously disturbed by the artillery magnetic field during launch. Moreover, the error parameters of the magnetometers, which are calibrated in advance, usually change after extended storage. The changed parameters have negative effects on attitude estimation of the projectile. To improve the accuracy of attitude estimation, the magnetometers should be calibr

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38

Stančić, Rade, and Stevica Graovac. "The integration of strap-down INS and GPS based on adaptive error damping." Robotics and Autonomous Systems 58, no. 10 (2010): 1117–29. http://dx.doi.org/10.1016/j.robot.2010.06.004.

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39

Mu-jun, Xie, Li Li-ting, and Wang Zhi-qian. "Study and Application of Variable Period Sampling in Strap-down North Seeking System." Energy Procedia 16 (2012): 2081–86. http://dx.doi.org/10.1016/j.egypro.2012.01.316.

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40

Fang, Tao, Weiquan Huang, Alan F. Lynch, and Zongyi Wang. "Non-damping system reset algorithm for shipborne grid strap-down inertial navigation systems." Measurement Science and Technology 31, no. 5 (2020): 055104. http://dx.doi.org/10.1088/1361-6501/ab6674.

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41

Cheng, Kai, Chun Mei Huang, and Yue Yuan Zhao. "Study on SRUKF Applied in Initial Alignment with Large Misalignment Angle on Stationary Base of SINS." Advanced Materials Research 383-390 (November 2011): 5088–93. http://dx.doi.org/10.4028/www.scientific.net/amr.383-390.5088.

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The initial alignment error model of SINS (Strap-down Inertial Navigation System) with large misalignment angle is nonlinear. The traditional EKF (Extended Kalman Filter) was used to linearization a nonlinear system, but its performance is limited. In this paper we use the SRUKF (Square Root Unscented Kalman Filter) to process this nonlinear system and the results indicate that SRUKF is better than EKF in convergence speed and estimation accuracy.

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42

Zhong, Run Wu, Shuai Chen, and Yu Kun Wang. "A Time Delay Compensation Algorithm for Transfer Alignment of Strap-Down Inertial Navigation System." Advanced Materials Research 909 (March 2014): 288–92. http://dx.doi.org/10.4028/www.scientific.net/amr.909.288.

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When SINS (slave strapdown inertial navigation system) got the MINS (Master Inertial Navigation System) data, the time reference was unified to the moment corresponding to the MINS data, and the data was processed by K'alman filter,which effects convergence speed and precision of airborne navigation system.In order to improve the precision of transfer alignment for airborne navigation system ,a compensation algorithm for information transmission time delay[1] is proposed to estimate the delay time and use relevant data to compensate the errors caused by time delay.A method using velocity and m

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43

Li, Xiang, and Zhi Li. "A new calibration method for tri-axial field sensors in strap-down navigation systems." Measurement Science and Technology 23, no. 10 (2012): 105105. http://dx.doi.org/10.1088/0957-0233/23/10/105105.

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44

Zhang, Henghao, Zaozhen Liu, Xiuyun Meng, and Yongwei Li. "The D-S theory algorithm with application in the strap-down inertial navigation system." International Journal of Modelling, Identification and Control 16, no. 3 (2012): 259. http://dx.doi.org/10.1504/ijmic.2012.047736.

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45

Sabatini, A. M. "Quaternion-based strap-down integration method for applications of inertial sensing to gait analysis." Medical & Biological Engineering & Computing 43, no. 1 (2005): 94–101. http://dx.doi.org/10.1007/bf02345128.

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46

Ben, Yue-yang, Yong-li Chai, Wei Gao, and Feng Sun. "Analysis of error for a rotating strap-down inertial navigation system with fibro gyro." Journal of Marine Science and Application 9, no. 4 (2010): 419–24. http://dx.doi.org/10.1007/s11804-010-1028-z.

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47

Xu, Zheng, Haibo Luo, Bin Hui, and Zheng Chang. "A Novel LOS Rate Estimation Method Based on Images for Strap-down Inertial Guidance." Journal of Physics: Conference Series 1570 (June 2020): 012060. http://dx.doi.org/10.1088/1742-6596/1570/1/012060.

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48

Qiu, Changzhen, Zhiyong Zhang, Huanzhang Lu, and Kaifeng Zhang. "Infrared modeling and imaging simulation of midcourse ballistic targets based on strap-down platform." Journal of Systems Engineering and Electronics 25, no. 5 (2014): 776–85. http://dx.doi.org/10.1109/jsee.2014.00090.

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Zhang, Qinglong, Bin Zhao, Yifu Jiang, Jingyan Zhang, and Jiale Zhang. "Integrated Guidance and Control for Strap-Down Flight Vehicle: A Deep Reinforcement Learning Approach." Aerospace 12, no. 5 (2025): 400. https://doi.org/10.3390/aerospace12050400.

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This paper proposes a three-dimensional (3D) deep reinforcement learning-based integrated guidance and control (DRLIGC) method, which is restricted by the narrow field-of-view (FOV) constraint of the strap-down seeker. By leveraging the data-driven nature of the deep reinforcement learning (DRL) algorithm, this method mitigates the challenges associated with integrated guidance and control (IGC) method design arising from model dependencies, thereby addressing the inherent complexity of the IGC model. Firstly, according to different states and actions, the pitch and yaw channels of the six-deg

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Bai, Shiyu, Weisong Wen, Yue Yu, and Li-Ta Hsu. "Invariant Extended Kalman Filtering for Pedestrian Deep-Inertial Odometry." International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences XLVIII-4-2024 (October 21, 2024): 607–12. http://dx.doi.org/10.5194/isprs-archives-xlviii-4-2024-607-2024.

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Abstract. Indoor localization for pedestrians, which relies solely on inertial odometry, has been a topic of great interest. Its significance lies in its ability to provide positioning solutions independently, without the need for external data. Although traditional strap-down inertial navigation shows rapid drift, the introduction of pedestrian dead reckoning (PDR), and artificial intelligence (AI) has enhanced the applicability of inertial odometry for indoor localization. However, inertial odometry continues to be affected by drift, inherent to the nature of dead reckoning. This implies tha

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