重复使用运载器末端区域能量管理段三维制导轨迹在线推演研究

张军;黄一敏;杨一栋

兵工学报 ›› 2010, Vol. 31 ›› Issue (1) : 41-47.

兵工学报 ›› 2010, Vol. 31 ›› Issue (1) : 41-47. DOI: 10.3969/j.issn.1000-1093.2010.01.009
论文

重复使用运载器末端区域能量管理段三维制导轨迹在线推演研究

  • 张军, 黄一敏, 杨一栋
作者信息 +

Research of Onboard 3-D Guidance Trajectory Propagation of Terminal Area Energy Management for RLVs

  • ZHANG Jun, HUANG Yi-min, YANG Yi-dong
Author information +
文章历史 +

摘要

研究了重复使用运载器(RLV)末端区域能量管理段(TAEM)三维制导轨迹在线推演算法。研究了重复使用运载器(RLV)末端区域能量管理段(TAEM)三维制导轨迹在线推演算法。根据RLV当前动压、位置和航向,规划动压参考剖面和横侧向参考轨迹,采用基于高度的质点动力学方程在线推演出满足过载、动压约束以及终点动压、位置和航向要求的三维轨迹。横侧向参考轨迹规划分为2个阶段,即消除横向位置误差兼顾减小纵向位置误差阶段和消除纵向位置误差阶段,提出了组合使用3种模态消除纵向位置误差的新方法。对于三维轨迹推演,提出了采用航迹倾斜角补偿法二次推演三维轨迹的新算法,修正终点位置误差超过自动着陆(ALI)容许范围的三维制导轨迹,使误差进入容许范围。仿真计算结果显示,该三维轨迹在线推演算法具有快速、准确、对初始点位置和航向分布鲁棒性强的特点。

Abstract

An onboard 3-D guidance trajectory algorithm of terminal area energy management

关键词

飞行器控制、导航技术 / 重复使用运载器 / 末端区域能量

Key words

control and navigation technology of aerocraft / reusable launch vehicle / termi

引用本文

导出引用
张军, 黄一敏, 杨一栋. 重复使用运载器末端区域能量管理段三维制导轨迹在线推演研究. 兵工学报. 2010, 31(1): 41-47 https://doi.org/10.3969/j.issn.1000-1093.2010.01.009
ZHANG Jun, HUANG Yi-min, YANG Yi-dong. Research of Onboard 3-D Guidance Trajectory Propagation of Terminal Area Energy Management for RLVs. Acta Armamentarii. 2010, 31(1): 41-47 https://doi.org/10.3969/j.issn.1000-1093.2010.01.009

参考文献

[1] BrindaV,Arora R K,Janardhana E. Mission analysis of a reus
able launch vehicle technology demonstrator (RLV-TD)[C]∥AIAA/CIRA 13th Inter
national Space Plants Hypersonics Systems and Technologies,US:American institu
te of aeronautics and Astronautics,2005,(3):2-7.
[2] MooreT E. Space shuttle entry terminal area energy management[M].
US:National Aeronautics and Space Administration,1991.
[3] HornemanK R,Kluever C A. Terminal, area energy management trajector
y planning for an unpowered reusable launch vehicle[C]∥AIAA Atmospheric Fligh
t Mechanics Conference and Exhibition,2004,(8):5-9.
[4] 孙春贞,黄一敏,郭锁凤.重复使用运载器末端能量管理段轨迹线设计[J]
.系统工程与电子技术,2007,29(6):910-914.
SUN Chun-zhen,HUANG Yi-min,GUO Suo-feng. Trajectory design for terminal are
a energy management of reusable launch vehicle[J].Systems Engineering and Elec
tronics,2007,29(6):910-914.(in Chinese)
[5] 孙春贞,黄一敏. 重复使用运载器末端区域能量管理轨迹鲁棒性分析[J].
兵工学报,2008,29(3):369-373.
SUN Chun-zhen,HUANG Yi-min. Robustness analysis of terminal area energy manag
ement trajectory for reusable launch vehicle[J].Acta Armamentarii,2008,29(3)
:369-373. (in Chinese)
[6] BartonG H,Grubler A C,Dyckman T R. New methodologies for onboard g
eneration of TAEM trajectories for autonomous RLVs[M]. Cambridge:The Charles
Stark Draper Laboratory,2002.
[7] BartonG H, Tragresser S G. Autolanding trajectory design for the X-
34[C]∥AIAA Atmospheric, Flight Mechanics Conference and Exhibit,Portland:OR
,1999:3-5.
[8] GrublerA C. New methodologies for onboard generation of terminal are
a energy management trajectories for autonomous reusable launch vehicle[D]. Ca
mbridge:Massachusetts Institute of Technology,2001.
[9] 沈宏良, 龚正. 航天飞机末端能量管理段在线轨迹设计方法[J].宇航学
报,2008,29(2):430-433.
SHEN Hong-liang,GONG Zheng. Methodology of onboard trajectory design for space
shuttle terminal area energy management phase[J]. Journal of Astronautics,20
08,29(2):430-433.(in Chinese)

文章所在专题

制导技术

315

Accesses

0

Citation

Detail

段落导航
相关文章

/