Yi Qiang Ji Zhang's Projects
One-dimensional Transient Heat Conduction in a semi-infinite Domain
Pork-Chop plot for Lambert's Problem of a Earth-Mars mission
This paper graphically presents the evolutions of several variables during the re-entry of two types of vehicles: Ballistic and Supporters
🛰️🚀A list of awesome space-related packages and resources maintained by The Orbital Index
This program will let you use bettercap easily. But before you have to install bettercap.
Webpage designed with space engineering APIs using React.js
Video, audio & banner adblock/skip for Spotify
The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.
First CSS styling
Developed an algorithm for Attitude Determination and control of a 1DOF 1U Cubesat.
Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)
This project aims to study the dynamic behavior of a simplified model of an aircraft when rolling (steady state) when it is circulating stationary on the runway. The roughness of the track is the main exciting agent that will be considered in this project.
Solutions to HackerRank practice, tutorials and interview preparation problems with Python 3, mySQL, C# and JavaScript
First HTML Page
Developed REST server using Raspberry Pi and SQLite and a further mobile interface with Cordova
Preliminary Design Of The Trajectory For An Interplanetary Mission Between Earth And Saturn With Natural Gravitatory Assistance From Jupiter
https://github.com/FedericoTartarini/reproducible-research/
Seven awesome latex ppt templates for researchers or students.
Mandelbrot set computation and visualization using Parallel processors (MPI) in C.
N-Body problem in C with parallel computing using 12 order Runge-Kutta with adaptive step size
Non-Linear Dynamic Systems
Numerical tools in Machine Learning for Aerospace Engineering
A LaTeX / XeLaTeX / LuaLaTeX PhD thesis template for Cambridge University Engineering Department (CUED)
Robotic Exploration of the Solar System using NASA's JPL SPICE Toolkit and Remote Sensing with LandSat 8 data
Parametric study of the vertical rise of a Rocket
This projects aims to use matrix calculus to determine the forces and displacements of the structures thus to obtain the stress state of each member of the bar, either traction (+) or compression (-).
The project aims to study the parametrical parameters of a two-spool turbofan with convergent nozzles
This is the Ultimate Windows 10 Script from a creation from multiple debloat scripts and gists from github.
Paper Air Challenge plane design
Yi Qiang Ji Zhang Portfolio
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