Abstract
The guidance technique presented in this study originates from the idea that it will be possible to impose the impact time against a moving target if the differential equation governing the behavior of the range can be made to have an analytical solution as a function of time. One direct way to do this involves two things, such as keeping the relative speed constant, and dictating a relative heading error profile that is composed of straight-line segments. The first item implies the application of the acceleration vector in a direction perpendicular to the relative velocity vector, while the second item, which is the key idea, gives rise to a multi-phased guidance structure).
Original language | English |
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Pages (from-to) | 1678-1685 |
Number of pages | 8 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 39 |
Issue number | 7 |
DOIs | |
State | Published - 2016 |