Accession Number : AD0482400
Title : EQUATIONS OF MOTION OF MISSILE WITH SLOSHING,
Corporate Author : THOMPSON RAMO WOOLDRIDGE INC LOS ANGELES CA
Personal Author(s) : Heist, E. K.
Report Date : 08 FEB 1956
Pagination or Media Count : 16
Abstract : The purpose is to derive the equations of motion, in two dimensions, of a rigid body missile with fluid sloshing, using the spring-mass analogy. These equations are arranged in a fashion most suitable for instrumentation in an analog computer simulation. Also of concern was the derivation of a transfer function relating missile attitude angle to motor deflection angle. From the resulting pole-zero configuration the closed loop system stability may then be determined. The coefficients of the transfer function are left in their most general form in terms of system parameters.
Descriptors : (*GUIDED MISSILES, EQUATIONS OF MOTION), (*SLOSHING, MOTION), SURFACE TO SURFACE MISSILES, LIQUID ROCKET FUELS, LIQUID ROCKET OXIDIZERS, AIRFRAMES, STRUCTURAL PROPERTIES, AERODYNAMIC CHARACTERISTICS, WIND, GRAVITY, COMPUTER PROGRAMMING, TWO DIMENSIONAL FLOW, ACCELERATION, ALTITUDE, CENTER OF GRAVITY, SIMULATION, FUNCTIONS(MATHEMATICS).
Subject Categories : Guided Missiles
Surface-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE