| 卫星编队队形保持非线性燃料次优控制 |
| |
| 引用本文： | 吴宝林,曹喜滨. 卫星编队队形保持非线性燃料次优控制[J]. 飞行力学, 2006, 24(1): 59-62 |
| |
| 作者姓名： | 吴宝林 曹喜滨 |
| |
| 作者单位： | 哈尔滨工业大学,卫星技术研究所,黑龙江,哈尔滨,150080 |
| |
| 基金项目： | 国家重点基础研究发展计划(973计划) |
| |
| 摘 要： | 针对卫星编队飞行队形保持推导了一种利用相对轨道根数为反馈量的非线性燃料次优控制算法。该控制算法基于高斯型摄动方程采用Lyapunov控制,控制增益是时变的以便控制某轨道根数时对其余的轨道根数影响最小。这种控制算法接近于燃料最优,且可以调整增益系数来适应推力大小的不同情况。仿真结果表明,该控制方法是有效的,且相比其他的控制算法能够节省更多的燃料。
|
| 关 键 词： | 队形保持 李亚普诺夫控制 增益选择 燃料次优控制 |
| 文章编号： | 1002-0853(2006)01-0059-04 |
| 收稿时间： | 2005-01-07 |
| 修稿时间： | 2005-12-19 |
Near Fuel-Optimal Nonlinear Control for Satellite Formation Keeping |
| |
| WU Bao-lin,CAO Xi-bin. Near Fuel-Optimal Nonlinear Control for Satellite Formation Keeping[J]. Flight Dynamics, 2006, 24(1): 59-62 |
| |
| Authors: | WU Bao-lin CAO Xi-bin |
| |
| Affiliation: | Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150080, China |
| |
| Abstract: | A near fuel-optimal control method for satellite formation keeping is developed.The orbit errors are expressed in terms of class orbit elements.Based on Gauss's variational equations of motion,the feedback control allows specific orbit elements to be controlled with minimal impact on the remaining orbit elements. Compared to optimal control solutions,the advantage of this control method is that it can operate with little computational effort and in a near fuel-optimal manner.Simulation results show that this control method is effective and can save more fuel than other methods. |
| |
| Keywords: | formation keeping Lyapunov control gain selection near fuel-optimal control |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
