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This paper describes the development procedure of a Six-Degree-of-Freedom simulation of a hypersonic cruise vehicle (HCV). The model and Computational Fluid Dynamics (CFD) simulation are developed to make conceptual design studies of hypersonic vehicles with scramjet. A description of the aerodynamic forces and moments system models formulated is included(More)
The aircraft cable fault location is a major task for the maintenance staffs. Based on the electric theory of distribution parameter circuit, a mathematical model of aircraft cable fault location is created. The principle of regression analysis is selected as the control algorithm because it has been applied successfully to parameter estimation. An aircraft(More)
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