Adaptive Secure Missile Guidance Against Additive and Multiplicative Cyber-Attacks
Author:
Affiliation:
1. Beihang University,School of Automation Science and Electrical Engineering,Beijing,P. R. China
2. Beihang University,Hangzhou Innovation Institute,Hangzhou,P. R. China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10587298/10587321/10587463.pdf?arnumber=10587463
Reference15 articles.
1. An Improvement in Three-Dimensional Pure Proportional Navigation Guidance
2. Capturability of Guidance Laws for Interception of Nonmaneuvering Target with Field-of-View Limit
3. A novel sliding mode guidance law without line-of-sight angular rate information accounting for autopilot lag
4. Time and FOV constraint guidance applicable to maneuvering target via sliding mode control
5. Adaptive reaching law based three-dimensional finite-time guidance law against maneuvering targets with input saturation
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