A Novel Guidance Law for Intercepting a Highly Maneuvering Target
Given the resolution of the guidance for intercepting highly maneuvering targets, a novel finite-time convergent guidance law is proposed, which takes the following conditions into consideration, including the impact angle constraint, the guidance command input saturation constraint, and the autopil...
| Published in: | International Journal of Aerospace Engineering |
|---|---|
| Main Authors: | , |
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-01-01
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| Online Access: | http://dx.doi.org/10.1155/2021/2326323 |