哈尔滨商业大学学报（自然科学版）Issue(6)：728-731,4.
高超声速飞行器上升段轨迹设计
Ascent trajectory design for hypersonic vehicle
摘要
Abstract
The trajectory design of hypersonic vehicle has many difficulties owing to the char-acteristics of itself.Hypersonic vehicle subjects to various constraints of aerodynamic,struc-ture and overload.In the ascent trajectory the effect is more obvious.Therefore,the design of hypersonic ascent trajectory needs to focus on these constraints.In this paper,based on these ideas,vehicle ’ s dynamics model and optimal control model were established, the optimal control model was transformed, and the hypersonic vehicle ascent trajectory was calculated. The results showed that the design method was reasonable and feasible,which could provide reference and help for similar work in the future.关键词
高超声速飞行器/飞行轨迹/序列二次规划法/结果仿真Key words
hypersonic vehicle/flight trajectory/sequential quadratic programming algo-rithm/simulated results分类
航空航天引用本文复制引用
王纯..高超声速飞行器上升段轨迹设计[J].哈尔滨商业大学学报（自然科学版）,2014,(6):728-731,4.
