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聂 涛
宇航学院
h-index
136
引用
6
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
2016
2024
每年的科研成果
概览
指纹图谱
合作网络
科研成果
(23)
相似学者
(1)
指纹图谱
深入其中 Tao Nie 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
Orbital Element
100%
Relative Distance
68%
Solar Radiation Pressure
65%
Long Term Evolution
65%
Simulation Result
64%
Semimajor Axis
56%
Computer Simulation
51%
Harmonics
45%
Perturbed Orbit
43%
Control Law
43%
Low Earth Orbit
37%
Image Plane
32%
Boundedness
32%
Multistage
32%
Optimization Approach
32%
Function of Time
32%
Particle Swarm Optimization
32%
Collision Risk
32%
Image Information
32%
Trajectory Planning
32%
Hamiltonian
32%
Matrix Theory
32%
Collision Avoidance
32%
Oblateness
32%
Local Cache
32%
Launch Vehicles
32%
Attitude Control
32%
Closed Form Expression
32%
Dynamical Equation
32%
Analytical Model
32%
Quadratic Function
32%
Body Effect
29%
Main Idea
27%
Space Object
25%
Orbital Plane
25%
Illustrates
23%
Orbital Transfer
21%
Safe Operation
18%
Feedback Control System
17%
Relative Motion
16%
Computational Time
16%
Satellite Formation Flying
16%
Success Rate
16%
Technical Challenge
16%
Phase Structure
16%
Circular Orbit
16%
Nonconvex Term
16%
Flight Dynamics
16%
Computational Efficiency
16%
Thruster
10%
Physics
Earth Orbit
98%
Satellite Formation
77%
Harmonics
67%
Formation Flying
65%
Solar Radiation
65%
Radiation Pressure
65%
Orbital Element
45%
Lunar Satellite
39%
SpaceX
36%
Mean Anomaly
32%
True Anomaly
32%
Satellite Orbit
32%
Continuity Equation
32%
Matrices (Mathematics)
32%
Atmospherics
32%
Satellite Formation Flying
27%
Lunar Orbit
19%
Von Zeipel Method
16%
Partial Differential Equation
16%
Earth Rotation
16%
Satellite Constellation
16%
Orbital Evolution
16%
Circular Orbit
16%
Semimajor Axis
13%
Feedback Control
6%
Earth and Planetary Sciences
Low Earth Orbit
94%
Satellite Formation
78%
Formation Flying
65%
Harmonics
38%
Solar Radiation
32%
Atmospherics
32%
Radiation Pressure
32%
Satellite Orbit
32%
Continuity Equation
32%
Lunar Satellite
32%
Collision Avoidance
32%
Real Time
32%
Satellite Constellation
19%
Lunar Orbit
19%
Von Zeipel Method
16%
Earth Rotation
16%
Orbital Element
6%
Feedback Control
6%
