Research on an extended composite proportional navigation law based on error adaptation and error anti saturation
DOI: 10.23977/jeis.2022.070401 | Downloads: 16 | Views: 484
Jing Yu 1, Junwei Lei 1, Hong Wang 1, Lingling Wang 1
1 College of Coast Defence, Naval Aviation University, Yantai, 264001, China
Corresponding AuthorJunwei Lei
According to the two-dimensional spatial relationship model of relative motion between missile and target, a constant value proportional navigation law based on error anti saturation is proposed on the basis of conventional proportional navigation and extended proportional navigation; Thirdly, the adaptive estimation design of guidance parameters is carried out from the angle error of longitudinal plane and lateral plane, angle coupling error, monocular distance, reciprocal of monocular distance and other aspects, and finally a composite three-dimensional proportional guidance method with error adaptation and error anti saturation is formed. The case digital simulation results also show the correctness and effectiveness of the proposed method.
KEYWORDSProportional guidance, Extended proportional navigation, Adaptive, Anti saturation, Miss distance
CITE THIS PAPER
Jing Yu, Junwei Lei, Hong Wang, Lingling Wang, Research on an extended composite proportional navigation law based on error adaptation and error anti saturation. Journal of Electronics and Information Science (2022) Vol. 7: 1-8. DOI: http://dx.doi.org/10.23977/jeis.2022.070401.
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