黄攀峰
个性化签名
- 姓名:黄攀峰
- 目前身份:
- 担任导师情况:
- 学位:
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学术头衔:
博士生导师, 教育部“新世纪优秀人才支持计划”入选者
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学科领域:
毛皮与制革工程
- 研究兴趣:
黄攀峰,教授,博士生导师。
1974年8月出生于陕西富平,分别于1998年7月,2001年3月获得西北工业大学航海学院获检测技术及仪器仪表专业学士学位和航天学院获导航、制导与控制专业硕士学位,2001年9月至2005年11月在香港中文大学自动化与计算机辅助工程系工作和攻读博士学位,师从于中国工程院院士、国际著名机器人专家、香港中文大学讲座教授徐扬生教授。2005年底加入西北工业大学,并破格晋升为副教授。2007年入选教育部“新世纪优秀人才” 支持计划;2008年1月起,担任国家863计划某重大项目专家组专家,2008年4月,破格晋升教授,2009年4月,被选聘为博士生导师,2009年9月起,担任某重大项目副总设计师;2011年获得中国人民解放军总装备部国家高技术研究计划(863计划)“十一五”先进个人称号。2012年获得军队科技进步一等奖一项(排第4)。2014年获得国防科学技术发明二等奖一项(排第1)
目前,主要从事新型空间机器人技术研究、空间机器人动力学与控制研究、智能技术、机器视觉、空间机器人遥操作技术方面的研究工作,近年来主持国家自然科学基金,国家863计划重大项目,教育部等20多项,在国内外重要期刊和重要国际会议上已发表学术论文70多篇,有60多篇论文被SCI或EI检索。出版《空间绳系机器人技术》和《空间遥操作技术》专著各一部。
招生方向:
空间机器人技术、空间遥操作技术、机器视觉、智能控制、导航、制导与控制等
联系办法: 029-88460366
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主页访问
4196
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关注数
0
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成果阅读
1021
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成果数
18
【期刊论文】On-line Estimation of Inertia Parameters of Space Debris for Its Tether-Assisted Removal
黄攀峰, Fan Zhang, Inna Sharf, Arun Misra, and Panfeng Huang*
ACTA Astronautica,-0001,():
-1年11月30日
This paper presents a new methodology for on-line inertia parameters estimation for a rigid space debris captured by a tethered system, based on a new dynamics model of the system where the base satellite (chaser) and the space debris (target) are modeled as rigid bodies and the attachment points of the tether are offset from the centers of mass of the two bodies. Parameters estimation of unknown debris is critical for subsequent tasks in the space debris remediation mission, in particular, for debris retrieval and de-orbiting. In the proposed algorithm, the chaser and target are modeled as rigid bodies, the latter with unknown inertia parameters. Then, the parameters identification problem is formulated and solved in three phases. First, a coarse estimate of the target mass is obtained during the post-capture phase, while the length of tether is much longer than the offsets of base and target satellite, and the rigid body model is degenerated to a mass point model. Then,with a proper tension control scheme and the coarse estimate used as an initial guess, the debris is retrieved smoothly and a precise mass estimate is achieved during the first halfof the retrieval. Finally, when the tether is retrieved relatively short and the rigid body model is used, moments of inertia and the offsets of the space debris will be estimated with a proper tension control scheme for rigid body model.
Space debris, Inertia parameters estimation, Tethered satellite system
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93浏览
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4下载
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【期刊论文】Dynamics and Configuration Control of the Maneuvering-Net Space Robot System
黄攀峰
Advances in Space Research,-0001,():
-1年11月30日
In order to eliminate the limitation of the Space Tether-Net System in the field of maneuver and control, we propose the Maneuvering-Net Space Robot System (MNSRS) in this paper, which can capture and remove the space debris dexterously. We focus on the approaching phase towards the space debris, which is a challenging problem for the MNSRS, especially the coupled dynamics modelling and configuration control problems. Firstly the system and mission overview of the MNSRS is described in detail. After that, a coupled dynamics modelling, which divides the MNSRS into finite mass points connected with massless springs, is established to describe dynamic characteristics of the MNSRS in approaching phase. Then the configuration variation of the MNSRS in approaching phase is analyzed. Finally the configuration control of the MNSRS in approaching phase is investigated.
Space Tether-Net System,, Approaching Maneuver,, Dynamics,, Configuration Control
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23浏览
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5下载
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【期刊论文】Coupling Dynamics Modelling and Optimal Coordinated Control of Tethered Space Robot
黄攀峰, Panfeng Huang*, Zehong Hu, and Zhongjie Meng
Aerospace Science and Technology,-0001,():
-1年11月30日
Tethered space robots use tethers to replace rigid arms and have more flexibility than a traditionalspace robot, which gives it wide application prospect in future on-orbit servicing missions. Before carrying out elaborate manipulations, tethered operation robots need to approach the target. In order to save fuel in the approaching phase, various coordinated control methods that employ tethers and thrusters together are investigated in the literature. However, the increasing mass of the tether and the distributed force acting on the tether will affect the position and attitude of the robot, which is neglected in previous studies and can degrade the performance of the control system. Here, in order to involve these factors, coupled dynamics and coordinated control theories are combined and applied. Firstly, a coupling dynamics model for the tethered space robot system is built based on the Hamilton principle and the linear assumption. Then, based on the dynamics model, we design an optimal coordinated controller which can minimize the fuel consumption by using the hp-adaptive pseudospectral method and the classical PD controller. Finally, the advantages of the proposed method and the performance of the designed controller are validated by the numerical simulation.
Tethered space robot, Dynamics modelling, Coordinated control, Optimal control
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36浏览
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5下载
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【期刊论文】Novel Method of Monocular Real-Time Feature Point Tracking for Tethered Space Robots
黄攀峰, Panfeng Huang, Jia Cai, Zhongjie Meng, Zehong Hu, and Dongke Wang
Journal of Aerospace Engineering,-0001,():
-1年11月30日
This paper proposes a visual perception system for a tethered space robot’s (TSR) automatic rendezvous from 100 to 0.15 m. The core problem, tracking the entire contour of noncooperative moving targets in real time, is emphasized in this work. Given numerous challenges in a dynamic scene, a novel feature tracking algorithm is developed, i.e., the monocular real-time robust feature tracking algorithm (MRRFT). To generate a robust target model, improved speeded-up robust features (SURF) are used to extract features from a marked target box. The tracker then uses the pyramid Kanade-Lucas-Tomasi (P-KLT) matching algorithm and eliminates mismatched points by a statistical method. The greedy snake algorithm is applied to obtain the exact location of the target box and to update it automatically. A discrete feature filter and an adaptive feature updating strategy are also designed to enhance robustness. A three-dimensional (3D) simulation and a semiphysical system are developed to evaluate the method. Numerous experiments demonstrate that the tracker can stably track satellite models with simple structures with improved accuracy and time savings than good features to track (GFTT)+P-KLT or scale invariant feature transform (SIFT)+P-KLT.
Tethered space robot system (, TSR), , Speeded-up robust features (, SURF), , Kanade-Lucas-Tomasi (, KLT), matching, Target tracking, Greedy snake.,
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47浏览
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5下载
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引用
黄攀峰, Panfeng Huang, Xiudong Xu and Zhongjie Meng
International Journal of Advanced Robotic Systems,-0001,():
-1年11月30日
The tethered space robot (TSR) is a new concept of space robot which consists of a robot platform, space tether and operation robot. This paper presents a multi-objective optimal trajectory planning and a coordinated tracking control scheme for TSR based on velocity impulse in the approaching phase. Both total velocity impulse and flight time are included in this optimization. The non-dominated sorting genetic algorithm is employed to obtain the optimal trajectory Pareto solution using the TSR dynamic model and optimal trajectory planning model. The coordinated tracking control scheme utilizes optimal velocity impulse. Furthermore, the PID controller is designed in order to compensate for the distance measurement errors. The PID control force is optimized and distributed to thrusters and the space tether using a simulated annealing algorithm. The attitude interferential torque of the space tether is compensated a using time-delay algorithm through reaction wheels. The simulation results show that the multi-objective optimal trajectory planning method can reveal the relationships among flight time, fuel consumption, planar view angle and velocity impulse number. This method can provide a series of optimal trajectory according to a number of special tasks. The coordinated control scheme can significantly save thruster fuel for tracking the optimal trajectory, restrain the attitude interferential torque produced by space tether and maintain the relative attitude stability of the operation robot.
Tethered Space Robot,, Velocity Impulse,, Optimal Trajectory,, Pareto Optimal Solutions,, Coordinated Control,, Time-delay
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96浏览
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4下载
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【期刊论文】Global Minimum-Jerk Trajectory Planning of Space Manipulator
黄攀峰, Panfeng Huang, Yangsheng Xu, and Bin Liang
International Journal of Control, Automation, and Systems, vol. 4, no. 4, pp. 405-413, August 2006,-0001,():
-1年11月30日
A novel approach based on genetic algorithms (GA) is developed to find a global minimum-jerk trajectory of a space robotic manipulator in joint space. The jerk, the third derivative of position of desired joint trajectory, adversely affects the efficiency of the control algorithms and stabilization of whole space robot system and therefore should be minimized. On the other hand, the importance of minimizing the jerk is to reduce the vibrations of manipulator. In this formulation, a global genetic-approach determines the trajectory by minimizing the maximum jerk in joint space. The planning procedure is performed with respect to all constraints, such as joint angle constraints, joint velocity constraints, joint angular acceleration and torque constraints, and so on. We use an genetic algorithm to search the optimal joint inter-knot parameters in order to realize the minimum jerk. These joint inter-knot parameters mainly include joint angle and joint angular velocities. The simulation result shows that GA-based minimum-jerk trajectory planning method has satisfactory performance and real significance in engineering.
Genetic algorithms,, minimum jerk,, space manipulator,, trajectory planning.,
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154浏览
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10下载
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【期刊论文】Minimum-torque Path Planning of Space Robots using Genetic Algorithms
黄攀峰, Panfeng Huang, Yangsheng Xu and Bin Liang
International Journal of Robotics and Automation.Vol.21 No.3, September, 2006(,-0001,():
-1年11月30日
Space robots will play a significant role in future space services. However, the energy supplied to the space robot system in space is limited because of the lower ratio of the solar panel. Therefore, the robotic manipulator’s trajectory should be optimum so that the torque of the manipulator can be minimized in order to save energy. This paper presents a minimum-torque path-planning scheme for space robots. In this formulation, a genetic-approach is used to minimize the objective function. The planning procedure is performed in joint space and with respect to all constraints, such as joint angle constraints, joint velocity constraints, joint angular acceleration and torque constraints, and so on. We use a genetic algorithm (GA) to search the optimal joint inter-knot parameters in order to realize the minimum-torque. These joint inter-knot parameters mainly include joint angle and joint angular velocities. The simulation results attest that GA-based minimum-torque path- planning method has satisfactory performance and real value.
Space robots,, path planning,, minimum-torque,, genetic algorithms
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60浏览
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8下载
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【期刊论文】Dynamic Balance Control of Multi-arm Free-Floating Space Robots
黄攀峰, Panfeng Huang, Yangsheng Xu and Bin Liang
International Journal of Advanced Robotic Systems,Vol.2 No.2 pp 117-124, June, 2005,-0001,():
-1年11月30日
This paper investigates the problem of the dynamic balance control of multi-arm free-floating space robot during capturing an active object in close proximity. The position and orientation of space base will be affected during the operation of space manipulator because of the dynamics coupling between the manipulator and space base. This dynamics coupling is unique characteristics of space robot system. Such a disturbance will produce a serious impact between the manipulator hand and the object. To ensure reliable and precise operation, we propose to develop a space robot system consisting of two arms, with one arm (mission arm) for accomplishing the capture mission, and the other one (balance arm) compensating for the disturbance of the base. We present the coordinated control concept for balance of the attitude of the base using the balance arm. The mission arm can move along the given trajectory to approach and capture the target with no considering the disturbance from the coupling of the base. We establish a relationship between the motion of two arm that can realize the zeros reaction to the base. The simulation studies verified the validity and efficiency of the proposed control method.
free-floating space robot,, dynamics,, dynamic control,, coordinated control.,
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69浏览
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8下载
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35浏览
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30浏览
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