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- W2355499916 abstract "The approximate solutions of the mid-course trajectories for the boost-glide vehicles are investigated.Firstly,with different assumptions,four types of approximate solutions are presented:(1)free flight solutions;(2) aero-controlled flight solutions with constant angle-of-attack;(3) the composite solution of the free flight and aero-controlled flight;(4) equilibrium glide solutions.Then the approximate solutions of mid-course trajectories are obtained by the combination of these solutions.The comparison between the approximate solutions and the numerical solutions validates the efficiency of this approach.Further more,the solutions of this paper is benefit for the estimation of the characteristics of this new trajectory,such as maximum heating rate,load factor and dynamic pressure during the period of the project demonstration." @default.
- W2355499916 created "2016-06-24" @default.
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- W2355499916 date "2007-01-01" @default.
- W2355499916 modified "2023-09-25" @default.
- W2355499916 title "Approximate Solutions of the Mid-Course Trajectories for the Boost-Glide Missiles" @default.
- W2355499916 hasPublicationYear "2007" @default.
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