An evaluation of the influence of distinct missile properties (acceleration phase, lead single constraints and maneuverability) and real world disturbances on the properties and requirements of collision course guidance is presented. For proportion navigation guidance, comprehensive diagrams are presented to evaluate the terminal miss behaviour, the requirements on the missile and on a line of sight angular rate measuring sensor. Missile dynamics, initial alignment errors, target maneuvers and target aspect-angle caused measurement errors were considered as real world disturbances.
The Collision Course: Conditions, Guidance Laws and Properties
1980
108 pages
Report
No indication
English
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