基于hp-自适应伪谱法的火星上升器精确入轨优化  

Optimization of Mars Ascent Vehicle orbit entry based on hp-adaptive pseudospectral method

作　　者：王浩朋 丁一波 岳晓奎[1,2,3] Wang Haopeng;Ding Yibo;Yue Xiaokui(School of Astronautics,Northwestern Polytechnical University,Xi'an 710072,China;Research&Development Institute of Northwestern Polytechnical University in Shenzhen,Shenzhen 518063,China;National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an 710072,China)

机构地区：[1]西北工业大学航天学院,西安710072 [2]西北工业大学深圳研究院,深圳518063 [3]西北工业大学航天飞行动力学技术重点实验室,西安710072

出　　处：《空天技术》2023年第6期53-65,共13页Aerospace Technology

基　　金：国家自然科学基金(12372048,12102343,U2013206);空间智能控制技术实验室开放基金课题资助(HTKJ2021KL502013);陕西省科学技术协会青年人才托举计划项目(20220509);航天飞行动力学技术重点实验室基金(KJW6142210210304);广东省基础与应用基础研究基金(2023A1515011421);中央高校基本科研业务费专项资金(D5000210833)。

摘　　要：针对火星表面上升器精确入轨任务场景,采用hp-自适应伪谱法对上升段轨迹进行优化。选择上升器构型为两级固液混合火箭加四个助推器,终端轨道为标准任务场景500 km圆轨道和火星环绕器所在中继椭圆轨道,得到上升时间和剩余质量以及终端轨道的实际入轨偏差。提出的上升器构型可显著减小上升段动压峰值。同时,考虑升交点赤径和近火点幅角约束的椭圆入轨情况,相比传统圆轨道可使上升器获得更高的入轨速度、更短的入轨时间以及更优的燃料消耗,并且在计算机中仿真验证耗时更短,适合实际工程应用。For the mission scenario of precise orbit insertion of the Mars surface ascent,the hp-adaptive pseudospectral method is used to optimize the trajectory of the ascent phase.The configuration of the ascent is a two-stage solid-liquid hybrid rocket with four boosters.The terminal orbit is the 500 km circular orbit of the standard mission scenario and the relay orbit where the Mars orbiter is located.The ascent time,residual mass,and actual orbital deviation of the terminal orbit are obtained.The proposed riser configuration can significantly reduce the peak dynamic pressure in the riser.Meanwhile,considering the elliptical orbit entry with the vertical diameter of the ascending node and the argument constraint of the argument of periareon compared with the traditional circular orbit,the ascent can obtain higher orbit entry speed,shorter orbit entry time and better fuel consumption,and the simulation and verification time in the computer is shorter,which is suitable for practical engineering applications.

关 键 词：火星上升器 hp-自适应伪谱法 采样返回 椭圆轨道 轨道六要素 精确入轨 

分 类 号：V229.7[航空宇航科学与技术—飞行器设计]