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Tao Nie
School of Aerospace Engineering
h-index
132
Citations
6
h-index
Calculated based on number of publications stored in Pure and citations from Scopus
2016
2024
Research activity per year
Overview
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Research output
(23)
Similar Profiles
(1)
Fingerprint
Dive into the research topics where Tao Nie is active. These topic labels come from the works of this person. Together they form a unique fingerprint.
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Weight
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Engineering
Analytical Model
32%
Attitude Control
32%
Body Effect
29%
Boundedness
32%
Circular Orbit
16%
Closed Form Expression
32%
Collision Avoidance
32%
Collision Risk
32%
Computational Efficiency
16%
Computational Time
16%
Computer Simulation
51%
Control Law
43%
Dynamical Equation
32%
Feedback Control System
17%
Flight Dynamics
16%
Function of Time
32%
Hamiltonian
32%
Harmonics
45%
Illustrates
23%
Image Information
32%
Image Plane
32%
Launch Vehicles
32%
Local Cache
32%
Long Term Evolution
65%
Low Earth Orbit
37%
Main Idea
27%
Matrix Theory
32%
Multistage
32%
Nonconvex Term
16%
Oblateness
32%
Optimization Approach
32%
Orbital Element
100%
Orbital Plane
25%
Orbital Transfer
21%
Particle Swarm Optimization
32%
Perturbed Orbit
43%
Phase Structure
16%
Quadratic Function
32%
Relative Distance
68%
Relative Motion
16%
Safe Operation
18%
Satellite Formation Flying
16%
Semimajor Axis
56%
Simulation Result
64%
Solar Radiation Pressure
65%
Space Object
25%
Success Rate
16%
Technical Challenge
16%
Thruster
10%
Trajectory Planning
32%
Physics
Atmospherics
32%
Circular Orbit
16%
Continuity Equation
32%
Earth Orbit
98%
Earth Rotation
16%
Feedback Control
6%
Formation Flying
65%
Harmonics
67%
Lunar Orbit
19%
Lunar Satellite
39%
Matrices (Mathematics)
32%
Mean Anomaly
32%
Orbital Element
45%
Orbital Evolution
16%
Partial Differential Equation
16%
Radiation Pressure
65%
Satellite Constellation
16%
Satellite Formation
77%
Satellite Formation Flying
27%
Satellite Orbit
32%
Semimajor Axis
13%
Solar Radiation
65%
SpaceX
36%
True Anomaly
32%
Von Zeipel Method
16%
Earth and Planetary Sciences
Atmospherics
32%
Collision Avoidance
32%
Continuity Equation
32%
Earth Rotation
16%
Feedback Control
6%
Formation Flying
65%
Harmonics
38%
Low Earth Orbit
94%
Lunar Orbit
19%
Lunar Satellite
32%
Orbital Element
6%
Radiation Pressure
32%
Real Time
32%
Satellite Constellation
19%
Satellite Formation
78%
Satellite Orbit
32%
Solar Radiation
32%
Von Zeipel Method
16%
