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| 六自由度飞行器编队建模与控制 | |
| 引用本文： | 赵刚,周琳莉,黄席樾.六自由度飞行器编队建模与控制[J].系统仿真学报,2011,23(10):2178-2183. |
| 作者姓名： | 赵刚 周琳莉 黄席樾 |
| 作者单位： | 1. 重庆大学自动化学院,重庆400044／第二炮兵驻重庆地区军事代表局,重庆400039 2. 后勤工程学院,重庆,400016 3. 重庆大学自动化学院,重庆,400044 |
| 基金项目： | 国家自然科学基金主任基金(60443006) |
| 摘 要： | 传统主从式编队常采用线性化反馈控制，很难满足复杂高精度空间飞行器编队要求。针对主从式飞行器相对平动和相对转动运动进行建模，进而得到统一的六自由度飞行器编从的非线性动力学模型。基于所得模型，设计了六自由度飞行器编队控制的滑模控制器和积分反推控制器，并给出基于Lyapunov的严格数学证明。仿真结果表明，控制器能够保证从飞行器六自由度运动跟踪误差的一致渐近收敛，为空间飞行器在轨服务等飞行器编队实际应用提供了理论参考。 |
| 关 键 词： | 飞行器编队控制 六自由度 建模 仿真 |
6 DOF Formation Flight Modeling and Control |
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| ZHAO Gang,ZHOU Lin-li,HUANG Xi-yue.6 DOF Formation Flight Modeling and Control[J].Journal of System Simulation,2011,23(10):2178-2183. | |
| Authors: | ZHAO Gang ZHOU Lin-li HUANG Xi-yue |
| Institution: | ZHAO Gang1,2,ZHOU Lin-li3,HUANG Xi-yue1(1.College of Automation,Chongqing University,Chongqing 400044,China,2.Chongqing Agent of Second Artillery Corps,PLA,Chongqing 400039,3.Logistical Engineering University,Chongqing 400016,China) |
| Abstract: | The relative translational and rotational dynamic models were established to meet the requirement of spacecraft high-precision formation flight.These models were further extended to a complete 6 DOF(Degree of Freedom) model.Based on this model,a sliding mode controller and an integral backstepping controller were developed,and rigid proofs based on Lyapunov theorem were given.Simulation results indicate that the designed controller can guarantee the closed loop system to be uniformly asymptotically stable(U... |
| Keywords: | spacecraft formation control 6DOF modeling simulation |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |