This report describes in detail a six-degree-of-freedom program which can be used to determine the trajectory and miss distance of a missile system. The options for the program are such as to permit variation of the aerodynamics, seeker, autopilot actuator and missile motor performance for the purpose of accurately simulating a given missile design and evaluating the effects of changes in system parameters. Sufficient detail has been included in the text in order to minimize the users' effort needed to know how to update or modify the program for his purposes. (Author)
Close Air Support Missile Guidance and Control Study. Volume I. Six-Degree-of-Freedom Simulation
1971
142 pages
Report
Keine Angabe
Englisch
Missile Technology , Computer Hardware , Laboratory & Test Facility Design & Operation , Guided missile simulators , Computer programs , Tactical air support , Close support , Air to air missiles , Guided missile trajectories , Air to surface missiles , Miss distance , Aerodynamics , Homing devices , Automatic pilots , Actuators , Solid propellant rocket engines , Subroutines , Simulation , Equations of motion , Passive systems , Lasers , Semiactive guidance , Six degree of freedom simulators
Tema Archiv | 1984
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