Study on Gyro Calibration and Attitude Estimation Considering an Induced Phase Anomaly Effect of High-Spin Maneuvering Body-Reference-Cited by-同舟云学术

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Study on Gyro Calibration and Attitude Estimation Considering an Induced Phase Anomaly Effect of High-Spin Maneuvering Body

Published:2024 Issue: Volume:73 Page:1-13
ISSN:0018-9456
Container-title:IEEE Transactions on Instrumentation and Measurement
language:
Short-container-title:IEEE Trans. Instrum. Meas.

Author:

Lee Juhwan¹^ORCID,Lee Byungjin²^ORCID,Sung Sangkyung³^ORCID

Affiliation:

1. Department of Aerospace Information Engineering, Konkuk University, Seoul, South Korea

2. Academy of Applied Science and Technology, Konkuk University, Seoul, South Korea

3. Department of Mechanical and Aerospace Engineering, Konkuk University, Seoul, South Korea

Funder

Korean National Research Fund

Unmanned Vehicles Core Technology Research and Development Program through the National Research Foundation of Korea

Korea Research Institute for Defense Technology Planning and Advancement (KRIT) Grant funded by the Korea Government [Defense Acquisition Program Administration (DAPA)]

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/19/10367905/10385144.pdf?arnumber=10385144

Reference46 articles.

1. Guidance and Control Design for a Class of Spin-Stabilized Fin-Controlled Projectiles

2. Flight Dynamics Modeling of Dual-Spin Guided Projectiles

3. A review of dual-spin projectile stability

4. Neural Network-Based Adaptive Control Design of Dual-Spin Projectile with Rotating Canards

5. Guidance and control for high dynamic rotating artillery rockets

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