Non-initial attitude error analysis of SINS by error closed-loop and energy-level constructing-Reference-Cited by-同舟云学术

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Non-initial attitude error analysis of SINS by error closed-loop and energy-level constructing

Published:2020-11 Issue: Volume:106 Page:106149
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Tang Chuanye

Funder

Senior Talent Foundation of Jiangsu University

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. A new second-order solution for strapped-down attitude computation;Savage,1966

2. An accurate strapdown direction cosine algorithm;Jordan,1969

3. A new concept in strapdown inertial navigation;Bortz,1969

4. Temperature drift modeling of MEMS gyroscope based on genetic-Elman neural network;Shen;Mech. Syst. Signal Process.,2016

5. A gyro signal characteristics analysis method based on empirical mode decomposition;Zeng;J. Sens.,2016

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Robust Attitude Estimation for Low-Dynamic Vehicles Based on MEMS-IMU and External Acceleration Compensation;Sensors;2024-07-17

2. An Improved Initial Alignment Method Based on SE2(3)/EKF for SINS/GNSS Integrated Navigation System with Large Misalignment Angles;Sensors;2024-05-06

3. A New Compressed-Structure-Based Coning Algorithm for Fiber Optic Strapdown Inertial Navigation Systems;IEEE Transactions on Instrumentation and Measurement;2021

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