Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty-Reference-Cited by-同舟云学术

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Robust-Backstepping Missile Autopilot Design Considering Time-Varying Parameters and Uncertainty

Published:2020-12 Issue:6 Volume:56 Page:4269-4287
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Lee Seokwon^ORCID,Kim Youdan^ORCID,Lee Yongwoo,Moon Gwanyoung,Jeon Byung-Eul

Funder

Agency for Defense Development

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

http://xplorestaging.ieee.org/ielx7/7/9280441/09079633.pdf?arnumber=9079633

Cited by 8 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. Addressing Launch and Deployment Uncertainties in UAVs with ESO-Based Attitude Control;Drones;2024-07-30

2. Gradient-Based Recursive Parameter Estimation Methods for a Class of Time-Varying Systems from Noisy Observations;Circuits, Systems, and Signal Processing;2024-07-29

3. Optimal Control Approach to Design a Three-Loop Autopilot for a Tactical Missile;Unmanned Systems;2024-04-03

4. Robust gain-scheduled missile autopilot design based on multifrequency extended state observers;Chinese Journal of Aeronautics;2023-12

5. A Generative Verification Framework on Statistical Stability for Data-Driven Controllers;IEEE Access;2023

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