Performance comparison of the notable acceleration- and angle-based guidance laws for a short-range air-to-surface missile

Date

2017-01-01

Author

Ozkan, Bulent
Özgören, Mustafa Kemal
Mahmutyazicioglu, Gokmen

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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Short-range air-to-surface missiles have become globally popular in the last two decades. As a performance driver, the type of guidance law gains importance. In this study, proportional navigation, velocity pursuit, and augmented proportional navigation guidance laws, whose resulting guidance commands take the form of lateral acceleration, are applied to a short-range air-to-surface missile against both stationary and maneuvering ground targets. Body pursuit and linear homing guidance laws, which yield angular commands, are additionally applied. Having completed the relevant computer simulations, we conclude that none of the acceleration- and angle-based guidance laws are absolutely superior to the others.

Subject Keywords

Guidance, Control, Short-range missile, Air-to-surface missile

URI

https://hdl.handle.net/11511/31159

Journal

TURKISH JOURNAL OF ELECTRICAL ENGINEERING AND COMPUTER SCIENCES

DOI

https://doi.org/10.3906/elk-1601-230

Collections

Graduate School of Natural and Applied Sciences, Article

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Citation Formats

B. Ozkan, M. K. Özgören, and G. Mahmutyazicioglu, “Performance comparison of the notable acceleration- and angle-based guidance laws for a short-range air-to-surface missile,” TURKISH JOURNAL OF ELECTRICAL ENGINEERING AND COMPUTER SCIENCES, pp. 3591–3606, 2017, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/31159.