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基于传热增广模型的轨迹优化与防热结构分析
引用本文:张腾飞,龚春林,粟华,薛鹏飞. 基于传热增广模型的轨迹优化与防热结构分析[J]. 系统工程与电子技术, 2022, 44(3): 929-938. DOI: 10.12305/j.issn.1001-506X.2022.03.25
作者姓名:张腾飞  龚春林  粟华  薛鹏飞
作者单位:1. 西北工业大学陕西省空天飞行器设计重点实验室, 陕西 西安 7100722. 空间物理重点实验室, 北京 100076
基金项目:国防科技创新特区(18H86303ZT001009004);国防基础科研项目(JCKY2020204B016)资助课题。
摘    要:在考虑飞行器结构温度约束的轨迹设计问题中,采用一般约束热流密度的轨迹优化模型存在反复迭代、不能考虑轨迹、传热之间耦合关系等缺点.针对这些问题,提出一种传热增广的轨迹优化模型.利用空间差分将传热方程转化为一阶微分方程组,与运动方程组成传热增广的系统状态方程,从而能在轨迹优化中对结构温度直接进行约束.算例仿真说明了基于增广...

关 键 词:轨迹优化  热传导  防热结构  高超声速
收稿时间:2021-06-08

Trajectory optimization based on heat-augmented model and analysis of thermal protection structure
ZHANG Tengafei,GONG Chunlin,SU Hua,XUE Pengfei. Trajectory optimization based on heat-augmented model and analysis of thermal protection structure[J]. System Engineering and Electronics, 2022, 44(3): 929-938. DOI: 10.12305/j.issn.1001-506X.2022.03.25
Authors:ZHANG Tengafei  GONG Chunlin  SU Hua  XUE Pengfei
Affiliation:1. Shannxi Aerospace Flight Vehicle Design Key Laboratory, Northwertern Polytechnical University, Xi'an 710072, China2. Science and Technology on Space Physics Laboratory, Beijing 100076, China
Abstract:In the trajectory design problem considering the temperature constraint of aircraft structure, the trajectory optimization model with general constrained heat flux has some disadvantages, such as repeated iteration, unable to consider the coupling relationship between trajectory and heat transfer. To solve these problems, a trajectory optimization model of heat transfer expansion is proposed. The heat transfer equation is transformed into a set of first-order differential equations by using spatial difference, and the system state equation of heat transfer expansion is formed with the motion equation, so that the structure temperature can be directly constrained in the trajectory optimization. The simulation of an example shows the efficiency of the solution based on the augmented model and the rationality of the result. On this basis, the interaction between reentry trajectory and thermal structure is analyzed, which provides a reference for the design of thermal structure in the scheme design stage.
Keywords:trajectory optimization  heat conduction  thermal protection structure  hypersonic
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