Publication Type : Research Article
Publisher : Sage Journals Home
Source : Journal of Aerospace Engineering
Url : https://journals.sagepub.com/doi/10.1177/09544100211046867
Campus : Coimbatore
School : Department of Aerospace Engineering, School of Engineering
Year : 2021
Abstract : This paper presents the nonstationary nonmaneuvering target interception with all possible desired impact angles in a two-dimensional (2D) aerial engagement scenario, where the target can move in any direction. The paper also considers the field-of-view (FOV) constraint for designing the guidance law so that the target is always visible while following the missile trajectory in the entire engagement time, which makes it feasible for real world applications. The guidance law is based on the pure proportional navigation (PPN) to achieve any impact angle of the entire angular spectrum. The proposed guidance law is then simulated for intercepting a nonstationary nonmaneuvering target using a kinematic model of a missile to demonstrate the efficacy of the presented scheme. A comparison with the related work existing in the literature has also been added to establish the superiority of the present work.
Cite this Research Publication : Singh NK, Hota S. FOV constrained guidance law for nonstationary nonmaneuvering target interception with any impact angle. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2022;236(10):1947-1960. doi:10.1177/09544100211046867