Kumar, Prem and Dwivedi, Prasiddha N and Bhattacharyya, Abhijit and Padhi, Radhakant (2017) Terminal-Lead-Angle-Constrained Generalized Explicit Guidance. In: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 53 (3). pp. 1250-1260.
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Abstract
Besides enhancing the warhead effectiveness, the terminal lead angle constraint ensures that the target remains within the field of view of the radio proximity fuse, which is very critical for the success of a mission. This paper presents substantial enhancement of the generalized explicit guidance to include the terminal lead angle constraint in three dimension (3-D).. With the availability of the desired total lead angle in 3-D, it computes the necessary terminal flight path and heading angles so that it not only satisfies the lead angle constraint, but also leads to the minimum among all minimum control effort solutions for various possible terminal flight path and heading angle combinations. With no lead angle constraint, it also gracefully degenerates to the standard proportional navigation guidance.
Item Type: | Journal Article |
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Publication: | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS |
Additional Information: | Copy right for this article belongs to the IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC, 445 HOES LANE, PISCATAWAY, NJ 08855-4141 USA |
Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
Date Deposited: | 15 Jul 2017 04:33 |
Last Modified: | 15 Jul 2017 04:33 |
URI: | http://eprints.iisc.ac.in/id/eprint/57394 |
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