Two-Stage Kalman Filter for Estimation of Wind Speed and UAV Flight Parameters based on GPS/INS and Pitot Tube Measurements
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/8760338/8767425/08767886.pdf?arnumber=8767886
Cited by 7 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
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2. A Non-Parametric Scheme for Identifying Data Characteristic Based on Curve Similarity Matching;IEEE/CAA Journal of Automatica Sinica;2024-06
3. Two-Stage Kalman Filter Based Estimation of Boeing 747 Actuator/Control Surface Stuck Faults;WSEAS TRANSACTIONS ON SIGNAL PROCESSING;2023-04-25
4. Wind Estimation using an H∞ Filter with Fixed-Wing Aircraft Flight Test Results;AIAA SCITECH 2023 Forum;2023-01-19
5. Flight Data-Based Wind Disturbance and Air Data Estimation;Atmosphere;2021-04-08
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