NDLI: A method to maneuver aeroballistic missiles under counteractions

Content Provider	Springer Nature Link
Author	Goncharenko, V. I. Gorchenko, L. D.
Copyright Year	2017
Abstract	A way to maneuver a high-speed aeroballistic missile (AMB) flying over an area where it can be shot down by enemy air and antimissile weapons is presented. It involves configuring the maneuver and setting reference points’ coordinates in a conditional coordinate system in advance. For setting the trajectory of an ABM with an anti-interception maneuver, the ABM is homed-in step-by-step to each reference point, whose coordinates are transformed in advance into a coordinate system connected with a certain area on the Earth. This offers the advantage of the possibility to plan maneuvers with any configuration without breaking the restrictions set on the controlling parameters.
Starting Page	505
Ending Page	518
Page Count	14
File Format	PDF
ISSN	10642307
Journal	Journal of Computer and Systems Sciences International
Volume Number	56
Issue Number	3
e-ISSN	15556530
Language	English
Publisher	Pleiades Publishing
Publisher Date	2017-07-01
Publisher Place	Moscow
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Control, Robotics, Mechatronics
Content Type	Text
Resource Type	Article
Subject	Applied Mathematics Theoretical Computer Science Computer Networks and Communications Control and Systems Engineering Information Systems Computer Vision and Pattern Recognition Software

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A method to maneuver aeroballistic missiles under counteractions