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Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile

  • Published:2010-11 Issue:6 Volume:33 Page:1801-1813
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Shaferman Vitaly1,Shima Tal1

Affiliation:

1. Technion—Israel Institute of Technology, Haifa 32000, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 128 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. Near-Optimal Evasion from Realistic Pursuers Employing Modern Linear Guidance Laws;AIAA SCITECH 2024 Forum;2024-01-04

2. Cooperative Nonlinear Aircraft Defense Using Super Twisting Algorithm with State Constraints;2023 62nd IEEE Conference on Decision and Control (CDC);2023-12-13

3. Capturability of the Pulsed Guidance Law Based on Differential Game Theory;2023 62nd IEEE Conference on Decision and Control (CDC);2023-12-13

4. Missile Threat Detection and Evasion Maneuvers With Countermeasures for a Low-Altitude Aircraft;IEEE Transactions on Aerospace and Electronic Systems;2023-12

5. Cooperative robust line‐of‐sight guidance law based on high‐gain observers for active defense;International Journal of Robust and Nonlinear Control;2023-07-10
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