固体火箭空间快速响应任务规划研究

doi:10.3969/j.issn.1009-086x.2021.01.015

摘要/Abstract

摘要： 针对空间快速响应任务中固体火箭弹道设计、微小卫星轨道规划相互独立,无法快速生成任务方案的问题,提出一种固体火箭空间快速响应任务规划方法。总结概述了空间快速响应任务规划的定义,在此基础上设计了固体火箭空间快速响应任务规划的总体架构,将其划分为任务要素分析、轨道规划、弹道规划、机动路径规划、方案评估和仿真演示共6个模块,阐述了各模块的功能,厘清了各模块之间的信息交互和制约关系,给出了各模块的实现方法和流程。研究结果可为固体火箭空间快速响应任务规划系统的实现奠定基础。

关键词: 固体火箭, 微小卫星, 空间快速响应, 任务规划, 总体架构, 模块划分

Abstract: To solve the problem of quick mission elements planning faced during operationally responsive space (ORS) because of the independence of trajectory of solid launch vehicle and microsatellite orbit design,a mission planning method of ORS for solid launch vehicle is proposed.Firstly,the definition of ORS mission planning is summarized.On the basis,the general framework of ORS mission planning based on solid launch vehicle is designed and divided into 6 modules,including factor analysis,orbit design,trajectory design,path planning,project evaluation and simulation.Then the functions are introduced and the information interaction and restrictive correlation between modules are teased out.Finally,the realization methods and working processes of modules are studied.The results of the study can provide reference for the development of ORS mission planning for solid launch vehicle.

Key words: solid launch vehicle, micro-satellite, operationally responsive space (ORS), mission planning, general framework, module division

中图分类号:

V553.2
TJ013

蔡应洲, 贺绍飞, 谷振丰, 闫郭伟. 固体火箭空间快速响应任务规划研究[J]. 现代防御技术, 2021, 49(1): 107-115.

CAI Ying-zhou, HE Shao-fei, GU Zhen-feng, YAN Guo-wei. Mission Planning of Operationally Responsive Space for Solid Launch Vehicle[J]. Modern Defense Technology, 2021, 49(1): 107-115.

参考文献

[1] MCCASLAND W N.Operationally Responsive Space (ORS)[C].Aerospace Conference IEEE,2006:1-2.
[2] 贺婷,梁波.美军太空安全与应急响应发展研究[J].指挥控制与仿真,2016,38(3):140-144.
HE Ting,LIANG Bo.Development of U.S.Military Space Security and Its Emergency Response[J].Command Control & Simulation,2016,38(3):140-144.
[3] 杨永峰,李明泽,钱军,等.航天快速发射内涵分析[J].导弹与航天运载技术,2016(5):44-47.
YANG Yong-feng,LI Ming-ze,QIAN Jun,et al.Connotation Analysis on the Aerospace Rapid Launch[J].Missiles and Space Vehicles,2016(5):44-47.
[4] 李兵,谷振丰,樊忠泽,等.基于贮存的固体运载火箭应急发射[J].导弹与航天运载技术,2016(S2):44-49.
LI Bing,GU Zhen-feng,FAN Zhong-ze,et al.Emergency Launch of Solid Launch Vehicle Based on Storage[J].Missiles and Space Vehicles,2016(S2):44-49.
[5] 彭科,胡凡,张为华.基于序列近似优化算法的固体运载火箭弹道设计[J].固体火箭技术,2017,40(2):250-256.
PENG Ke,HU Fan,ZHANG Wei-hua.Solid Launch Vehicles Trajectory Design Based on Sequential Approximate Optimization Algorithm[J].Journal of Solid Rocket Technology,2017,40(2):250-256.
[6] 张迁,许志,李新国.一种多级全固体运载火箭上升段自主制导方法[J].宇航学报,2019,40(1):19-28.
ZHANG Qian,XU Zhi,LI Xin-guo.An Autonomous Ascent Guidance Method for Multi-Stage Solid Launch Vehicles[J].Journal of Astronautics,2019,40(1):19-28.
[7] CHANDLER P R,PACHTER M,RASMUSSEN S.UAV Cooperative Control[C]//2001 American Control Conference,2001:50-55.
[8] 沈林成,陈璟,王楠.飞行器任务规划技术综述[J].航空学报,2014,35(3):593-606.
SHEN Lin-cheng,CHEN Jing,WANG Nan.Overview of Air Vehicle Mission Planning Techniques[J].Acta Aeronautica et Astronautica Sinica,2014,35(3):593-606.
[9] 赵田,张炜,吕耀平.任务规划系统发展现状与启示[J].装备学院学报,2016,27(2):30-33.
ZHAO Tian,ZHANG Wei,LÜ Yao-ping.Development and Enlightenment of Mission Planning System[J].Journal of Equipment Academy,2016,27(2):30-33.
[10] 杨萍,刘卫东,李德龙,等.常规导弹作战任务规划系统设计与实现[J].火力与指挥控制,2014,39(3):151-154.
YANG Ping,LIU Wei-dong,LI De-long,et al.Design and Implementation of Mission Planning System of Conventional Missile Operational[J].Fire Control & Command Control,2014,39(3):151-154.
[11] 赵国宏,罗雪山.作战任务规划系统研究[J].指挥与控制学报,2015,1(4):391-394.
ZHAO Guo-hong,LUO Xue-shan.On Operation Mission Planning System[J].Journal of Command and Control,2015,1(4):391-394.
[12] 王晓晖,李爽.深空探测器约束简化与任务规划方法研究[J].宇航学报,2016,37(7):768-774.
WANG Xiao-hui,LI Shuang.Research on Constraint Simplification and Mission Planning Method for Deep Space Explorer[J].Journal of Astronautics,2016,37(7):768-774.
[13] 张道昶,樊忠泽.固体火箭应急发射任务规划及发射流程研究[J].现代防御技术,2018,46(6):122-128.
ZHANG Dao-chang,FAN Zhong-ze.Research on Mission Planning and Launch Flow of Solid Rocket Emergency Launch[J].Modern Defence Technology,2018,46(6):122-128.
[14] 贺绍飞,谷振丰,李明泽,等.快速响应太阳同步轨道/发射窗口一体规划[J].航天控制,2019,37(5):51-55.
HE Shao-fei,GU Zhen-feng,LI Ming-ze,et al.Integrated Design of Operationally Responsive Sun-Synchronous Orbit and Launch Time[J].Aerospace Control,2019,37(5):51-55.
[15] 韩潮,邓丽,徐嘉.星座覆盖性能评估的改进网格点仿真法[J].计算机仿真,2005,22(12):21-23.
HAN Chao,DENG Li,XU Jia.Improved Grid Simulation for Constellation Coverage Performance Evaluation[J].Computer Simulation,2005,22(12):21-23.
[16] 莫宇,闫大伟,游鹏,等.通信卫星星座优化设计综述[J].电讯技术,2016,56(11):1293-1300.
MO Yu,YAN Da-wei,YOU Peng,et al.A Survey of Constellation Optimization Design for Satellite Communications[J].Telecommunication Engineering,2016,56(11):1293-1300.
[17] 王励,王炎娟,张辉,等.基于NGSA-Ⅱ算法的区域覆盖卫星星座优化[J].计算机仿真,2009,26(4):80-84.
WANG Li,WANG Yan-juan,ZHANG Hui,et al.Optimizaiton of Regional Coverage Reconnaissance Satellite Constellations by NSGA-Ⅱ Algorithm[J].Computer Simulation,2009,26(4):80-84.
[18] 蒙波,伊成俊,韩潮.基于多目标粒子群算法的导航星座优化设计[J].航空学报,2009,30(7):1285-1291.
MENG Bo,YI Cheng-jun,HAN Chao.Optimization of Navigation Satellite Constellation by Multi-objective Particle Swarm Algorithm[J].Acta Aeronautica et Astronautica Sinica,2009,30(7):1285-1291.
[19] 付晓锋.空间快速响应任务中的轨道设计问题研究[D].长沙:国防科学技术大学,2011.
FU Xiao-feng.Orbit Design in Responsive Space Missions[D].Changsha:National University of Defense Technology,2011.
[20] 张柳,张雪梅,唐琼,等.基于组合粒子群算法的运载火箭弹道优化设计[J].导弹与航天运载技术,2016(6):1-5.
ZHANG Liu,ZHANG Xue-mei,TANG Qiong,et al.Using a Hybrid Algorithm Based on Particle Swarm Optimization for Launch Vehicle Trajectory Optimization[J].Missile and Space Vehicles,2016(6):1-5.
[21] 李晓苏,晁涛,王松艳.基于鱼群算法的运载火箭上升段弹道优化设计[J].系统仿真学报,2018,30(12):4747-4753.
LI Xiao-su,CHAO Tao,WANG Song-yan.Trajectory Optimization Design of Ascending Phase for Solid Launch Vehicle Based on Fish-swarm Algorithm[J].Journal of System Simulation,2018,30(12):4747-4753.
[22] 马特,刘刚,何兵.弹载小卫星应急发射入轨方法设计与优化[J].现代防御技术,2018,46(3):177-183.
MA Te,LIU Gang,HE Bing.Design and Optimization of the Method of Launching the Small Satellite by Missile Under Emergency[J].Modern Defense Technology,2018,46(3):177-183.
[23] 王美玲,潘允辉.基于GIS与约束条件下的最优路径规划研究[J].北京理工大学学报,2016,36(8):851-856.
WANG Mei-ling,PAN Yun-hui.Research on Optimal Path Planning with Constraints Based on GIS[J].Transactions of Beijing Institute of Technology,2016,36(8):851-856.
[24] 刘凯,吕晓华,李爱光,等.摩托化机动路径规划的改进A*算法[J].测绘科学技术学报,2017,34(5):545-550.
LIU Kai,LÜ Xiao-hua,LI Ai-guang,et al.Research on Improved A* Algorithm for Motorized Path Planning of Motorized[J].Journal of Geomatics Science and Technology,2017,34(5):545-550.
[25] 程呈,高敏,程旭德,等.基于组合赋权的反坦克导弹武器系统作战效能评估研究[J].系统工程理论与实践,2018,38(1):241-251.
CHENG Cheng,GAO Min,CHENG Xu-de,et al.Research on Operational Efficiency Evaluation of Anti-tank Missile Weapon System Based on Combination Weighting[J].Systems Engineering—Theory & Practice,2018,38(1):241-251.
[26] 陈汗龙,吴晓朝,赵明洋,等.基于TOPSIS算法的防空通信网络系统效能评估[J].火力与指挥控制,2016,41(7):140-143.
CHEN Han-long,WU Xiao-chao,ZHAO Ming-yang,et al.TOPSIS-based Effectiveness Evaluation of Air Defense Communication Network System[J].Fire Control & Command Control,2016,41(7):140-143.
[27] 刘国强,陈维义,程晗,等.基于BP神经网络的炮光集成武器系统作战效能评估与预测[J].海军工程大学学报,2019,31(3):55-59.
LIU Guo-qiang,CHEN Wei-yi,CHENG Han,et al.Evaluation and Prediction of Combat Effectiveness on Weapon System with Gun and Laser Based on BP Networks[J].Journal of Naval University of Engineering,2019,31(3):55-59.
[28] 李波,雒浩然,田琳宇,等.基于DBN效能拟合的舰艇编队作战效能敏感性分析[J].航空学报,2019,40(12):156-166.
LI Bo,LUO Hao-ran,TIAN Lin-yu,et al.Sensitivity Analysis of Ship Formation Operational Effectiveness Based on DBN Effectiveness Fitting[J].Acta Aeronautica et Astronautica Sinica,2019,40(12):156-166.