| 引用本文: | 胡建学,陈克俊,赵汉元,等.RLV再入标准轨道制导与轨道预测制导方法比较分析.[J].国防科技大学学报,2007,29(1):26-29,34.[点击复制] |
| HU Jianxue,CHEN Kejun,ZHAO Hanyuan,et al.Comparisons Between Reference-trajectory and Predictor-corrector Entry Guidances for RLVs[J].Journal of National University of Defense Technology,2007,29(1):26-29,34[点击复制] |
|
| |
|
|
| 本文已被：浏览 7094次 下载 5875次 |
| RLV再入标准轨道制导与轨道预测制导方法比较分析 |
| 胡建学1, 陈克俊1, 赵汉元1, 余梦伦2 |
|
(1.国防科技大学 航天与材料工程学院，湖南 长沙 410073;2.中国运载火箭研究院 总体设计部，北京 100076)
|
| 摘要: |
| 提出只更新飞行剖面参数的航程更新方法及相应的RLV再入标准轨道制导规律；结合轨道在线生成与跟踪技术，采用Runge-Kutta-Fehlberg自适应变步长轨道快速预报方法，研究了RLV再入轨道预测制导。进一步对两种制导方法进行了比较分析研究，研究认为标准轨道制导与轨道预测制导都是可行的RLV再入制导方案，其有机结合是未来可重复使用跨大气层飞行器再入制导的发展趋势。 |
| 关键词: 可重复使用运载器（RLV） 再入制导 标准轨道制导 预测制导 |
| DOI： |
| 投稿日期：2006-09-23 |
| 基金项目:国家863基金资助项目(2004AA721073) |
|
| Comparisons Between Reference-trajectory and Predictor-corrector Entry Guidances for RLVs |
| HU Jianxue1, CHEN Kejun1, ZHAO Hanyuan1, YU Menglun2 |
|
(1.College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;2.Systems Engineering Division, China Academy of Launch Vehicle Technology, Beijing 100076, China)
|
| Abstract: |
| A new reusable launch vehicle (RLV) entry guidance algorithm with ranging technique which only needs to update flight profile parameters was developed and a predictor-corrector entry guidance methodology using Runge-Kutta-Fehlberg method for RLVs combined with trajectory online generation technology was studied. Comparisons between the two guidance schemes were performed, and simulation results show that the two guidance methods are feasible, which indicates that the integration of reference-trajectory entry guidance and predictor-corrector entry guidance is a promising entry guidance scheme for future RLVs. |
| Keywords: reusable launch vehicle entry guidance reference-trajectory guidance predictor-corrector guidance |
|
|
|
|
|
