
Accession Number : AD0283911
Title : SIXDEGREEOFFREEDOM EQUATIONS OF MOTION FOR A MANEUVERING REENTRY VEHICLE
Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY
Personal Author(s) : SCHULER, JOHN M. ; PRITCHARD, FRANCIS E.
PDF Url : AD0283911
Report Date : 15 JUN 1962
Pagination or Media Count : 180
Abstract : Equations of motion for a reentry vehicle are developed for use with a digitally operated, fixedbase simulator. The equations provide: six degreesoffreedom for a vehicle of nonvarying mass hose trajectory and orientationARE GIVEN WITH RESPECT TO A SPHERICAL, ROTATING EARTH; AN INVERSE SQUARE GRAVITATIONAL FORCE, A ROTATING ATMOSPHERE, AND RELEVANT ATMOSPHERIC PROPERTIES; AND AERODYNAMIC FORCES AND MOMENTS IN COEFFICIENT FORM, AND REACTION CONTROL MOMENTS. The only restriction on attitude, maneuver, or flight path is that flights directly over the North and South poles are excluded. The equations, as described, have been programme on an IBM 704 and specific solutions were obtained to show effects of maneuvers, pilot's inputs, different geophysical models, and mathematical simplifications. The report contains descriptive chapters on geophysics and aerodyn mics and control which are especially pertinent to reentry simulation. In addition, Appendices extend the equations for varying mass, large thrust, and earth oblateness with rela ed effects.
Descriptors : *ATMOSPHERE ENTRY, *DEGREES OF FREEDOM, *REENTRY VEHICLES, MATRICES(MATHEMATICS), THEORY, MOMENTS, AERODYNAMIC CHARACTERISTICS, PERTURBATION THEORY, GRAVITY, EQUATIONS, GEOPHYSICS, DIGITAL COMPUTERS, CELESTIAL MECHANICS, MANEUVERABILITY, SIMULATION, ENERGY MANAGEMENT, CONTROL
Subject Categories : Statistics and Probability
Guided Missile Reentry Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE