Three-dimensional Multi-missile Cooperative Guidance Law with Time and Space Constraints
Author:
Affiliation:
1. Northwestern Polytechnical University,School of Electronics and Information,Xi’an,China,710072
2. The First Military Representative Office of the Air Force Equipment,Department in Chengdu,Chengdu,China,610000
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10003266/10003667/10003825.pdf?arnumber=10003825
Reference11 articles.
1. Consensus-Based Two-Stage Salvo Attack Guidance
2. Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems
3. Three-dimensional adaptive fixed-time cooperative guidance law with impact time and angle constraints
4. Finite‐time cooperative guidance laws for multiple missiles with acceleration saturation constraints
5. Guidance law to control impact time and angle;lee;IEEE Transactions on Aerospace and Electronic Systems,2007
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1. Multi-Missile Cooperative Guidance Law Under Communication Delay and Topological Transformation in 3-D;2023 5th International Conference on Control and Robotics (ICCR);2023-11-23
2. A Fixed-Time Convergence Adaptive Fast Sliding Mode Guidance Law with Angle Constraint;2023 11th International Conference on Control, Mechatronics and Automation (ICCMA);2023-11-01
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