跳到主要导航
跳到搜索
跳到主要内容
北京理工大学 首页
English
中文
首页
师资队伍
研究单位
科研成果
奖项
按专业知识、名称或附属进行搜索
查看 Scopus 资料
周 星宇
机械与车辆学院
h-index
156
引用
9
H-指数
根据储存在 Pure 的刊物以及来自 Scopus 的引用文献数量计算
2021
2024
每年的科研成果
概览
指纹图谱
合作网络
科研成果
(25)
相似学者
(4)
指纹图谱
深入其中 Xingyu Zhou 为活跃的研究主题。这些主题标签来自此人的成果。它们共同形成唯一的指纹。
分类
加权
按字母排序
Engineering
Orbit Determination
100%
Observability
36%
State Transition
35%
Cooperative
33%
Deep Neural Network
22%
Extended Kalman Filter
21%
Long Short-Term Memory
20%
Kalman Filter
17%
Computer Simulation
17%
Optimisation Problem
16%
Design Analysis
11%
Breathing
11%
Orbital Element
11%
Domain Analysis
11%
Nonlinearity
11%
Convolutional Neural Network
11%
Distributed Control
11%
Optimal Design
11%
Detection Algorithm
11%
Roundtrip
11%
Collision Avoidance
11%
Term Stability
11%
Reconfiguration
11%
Relative Error
11%
Surrogate Model
11%
Stability Analysis
11%
Powertrain
11%
Impulsive Maneuver
11%
Directional
11%
Initial Guess
9%
Antenna
8%
Computational Time
8%
Laser Interferometer
8%
Corrector
7%
Low Earth Orbit
6%
Electric Vehicle
6%
Feature Extraction
5%
Angular Momentum
5%
Infrastructure
5%
Delay Time
5%
Rigid Structure
5%
Genetic Algorithm Method
5%
Optimization Method
5%
Initial Configuration
5%
Nonlinear Problem
5%
Parameter Uncertainty
5%
Double Layer
5%
Design Problem
5%
Numerical Optimization
5%
External Disturbance
5%
Computer Science
Optimization Framework
16%
Greedy Algorithm
11%
Task Execution
11%
Detection Algorithm
11%
Deep Neural Network
11%
Mixed Integer Programming
11%
Mobile Robot
11%
Kalman Filtering
11%
Planning Method
11%
Optimization Problem
11%
Final Solution
11%
Convolutional Neural Network
11%
Differential Evolution
11%
Nonlinear Programming
11%
Design Problem
11%
Mobile Robot Systems
8%
Genetic Algorithm
5%
Feature Extraction
5%
Numerical Simulation
5%
Robot
5%
Information Storage
5%
Computational Time
5%
Optimal Assignment
5%
Computation Cost
5%
Classifier
5%
Layer Optimization
5%
Performance Optimization
5%
Reconfiguration Problem
5%
Physics
Gravitational Wave
48%
Spacecraft
28%
Orbit Determination
22%
Orbit Insertion
21%
Orbital Mechanics
11%
Orbital Element
11%
Observatory
11%
Antenna
6%
Apparent Magnitude
5%
Sun
5%
