国防科技大学学报2018，Vol.40Issue(3)：1-6,6.DOI:10.11887/j.cn.201803001
翼伞系统线目标归航方法
Line target homing method of parafoil system
摘要
Abstract
Aimed to the large dispersion situation of the rocket booster or sub-stage falling to the ground without controlling, the line target homing method of parafoil system was put forward.The calculation model of rectangular boundary was established, and the contraction regional analysis of two kinds of homing methods namely point target and target line was performed.The influence of parafoil homing ability and the scattered boundary characteristics of falling area on homing performance were analyzed, and the corresponding homing strategy was obtained.A solution for setting up multiple landing areas in larger dispersion area was proposed.Finally, the dynamics and control model was established and the line target homing process was simulated.Satisfactory results are obtained,which shows that the proposed method has some reference value to the project.关键词
翼伞/线目标/归航控制/仿真/落区控制/路径规划Key words
parafoil/line target/homing control/simulation/landing zone control/path planning分类
航空航天引用本文复制引用
滕海山,汤国建,刘涛,张章..翼伞系统线目标归航方法[J].国防科技大学学报,2018,40(3):1-6,6.基金项目
国家自然科学基金青年科学基金资助项目(11602018) （11602018）
