BASIC CONSIDERATIONS IN THE DEVELOPMENT OF AN UNGUIDED ROCKET TRAJECTORY SIMULATION MODEL
作者： Louis D Duncan
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摘要: Abstract : The basic requirements for the development of a six-degree-of-freedom digital simulation model are outlined, and three coordinate systems specified which both adequate convenient such development. nontrivial transformations shown. equations motion developed, with indications standard assumptions. principal forces moments discussed. thrust misalignment effects derived formulas jet damping moment included. Aerodynamic discussed, necessary aerodynamic angles defined. These described from stability derivative point view, components major derived.
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