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RLV末端能量管理段轨迹优化与纵向控制律设计 被引量:2

Trajectory optimization and longitudinal control for terminal area energy management of reusable launch vehicle
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摘要 末端能量管理段的目的是控制RLV的能量,使其能够以合适的能量状态进入自动着陆窗口,以保证最终能够安全着陆。重点是满足飞行过程中的物理约束和自动着陆窗口终端约束的轨迹规划和轨迹跟踪。本文首先将轨迹规划转化为优化问题,然后给出能量走廊之内的能量剖面跟踪策略,最后设计纵向轨迹跟踪控制律并进行仿真。仿真结果表明此方法能够设计出合理的下滑轨迹并进行跟踪,跟踪精度较高。 Managing the energy of reusable launch vehicle(RLV) to make it arrive the auto-landing interface and ensure that RLV can land safely, it’s the main purpose of terminal area energy management(TAEM). The emphases are trajectory programming and tracking that can meet the physical?and auto-landing interface constraints. In this article, trajectory programming is transformed into an optimized problem.Then the trajectory tracking method is built. At last, the trajectory tracking law is designed. The simulations show the method mentioned above can give a reasonable?trajectory with a high tracking precision.
出处 《电子设计工程》 2014年第20期42-44,48,共4页 Electronic Design Engineering
关键词 末端能量管理 能量走廊 轨迹规划 轨迹跟踪 TAEM energy corridor trajectory programming trajectory tracking
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参考文献5

  • 1Barton G H,Tragresser S. G.Autolanding Trajectory Design for the X-34 [C]//AIAA,August 1999:99-4146.
  • 2Barton, G. H,New Methodologies for Assessing the Robust- ness of the X-34 Autolanding Trajectories[C]//American As- tronautical Society,2001:1-14.
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  • 4Girerd,A. R,Onboard Trajectory Generation for the Unpow- ered Landing of Autonomous Reusable Launch Vehicles [D]. S.M. Thesis,Department of Aeronautics and Astronautics, M1T,2001.
  • 5沈宏良,陶矩,魏立新,刘昶.航天飞机自动着陆轨迹优化设计[J].飞行力学,2004,22(1):10-13. 被引量:6

二级参考文献1

  • 1赵汉元.飞行器再入动力学和制导[M].长沙:国防科技大学出版社,1997..

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