Accession Number : ADA298296
Title : Simulink Simulation of Proportional Navigation and Command to Line of Sight Missile Guidance.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Costello, Patrick
PDF Url : ADA298296
Report Date : MAR 1995
Pagination or Media Count : 88
Abstract : Proportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-dimensional engagement and two three-dimensional engagement scenarios. The final three-dimensional scenario introduces measurement noise in order to evaluate the effect of noise on the guidance algorithms. The engagement results are then compared to analyze the miss distance of each type of missile guidance.
Descriptors : *LINE OF SIGHT, *GUIDED MISSILES, *GUIDANCE, *PROPORTIONAL NAVIGATION, ALGORITHMS, SCENARIOS, CONTROL, SIMULATION, MEASUREMENT, THREE DIMENSIONAL, SIGHTS, FLOW CHARTING, NOISE, TRANSFER, MISS DISTANCE.
Subject Categories : Guided Missiles
Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE