Yajur Kumar
Indian Space Research Organisation
Technical Articles at www.spacenavigators.com, Masters from IIT Kanpur in Aerospace Engineering, work as AOCS and GNC Engineer at ISRO's Satellite Centre
Python, C++, C, MATLAB
Spoken Languages:
English, Hindi
Pronouns:
He/him
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Submitted
Dynamically Tuned Gyroscope Simulator
Dynamically Tuned Gyroscope Simulator
1 year ago | 2 downloads |
Submitted
Implementation of State Observer in Spring Mass Damper
This MATLAB code simulates and animates a mass-spring-damper system with a Luenberger observer.
2 years ago | 5 downloads |
Submitted
Control of Inverted Pendulum in a Cart using MPC
Controlling an inverted pendulum using MPC, covering the essential concepts and implementation with animation.
2 years ago | 6 downloads |
Submitted
Robotic Manipulator Transformation Matrix
Function to compute homogeneous transformation matrix from base to end effector for a robotic manipulator
3 years ago | 1 download |
Submitted
Classical Orbit Elements to Position Velocity Vector
Convert Classical Orbital Elements to Position Velocity Vector in ECI Frame and vice-versa
3 years ago | 8 downloads |
Issues running Simulink/MATLAB when running batch file for FlightGear
I had the same issue previously. It can be solved by running the FlightGear batch file 'runfg.bat' directly from the windows exp...
7 years ago | 1
Solved
Make the vector [1 2 3 4 5 6 7 8 9 10]
In MATLAB, you create a vector by enclosing the elements in square brackets like so: x = [1 2 3 4] Commas are optional, s...
7 years ago
Solved
Pernicious Anniversary Problem
Since Cody is 5 years old, it's pernicious. A <http://rosettacode.org/wiki/Pernicious_numbers Pernicious number> is an integer w...
7 years ago
Solved
Energy of a photon
*⚛ ☢ ⚛ ☢ ⚛ ☢ ⚛* Given the frequency F of a photon in giga hertz. Find energy E of this...
7 years ago
Solved
How to subtract?
*± ± ± ± ± ± ± ± ± ± ±* * Imagine you need to subtract one...
7 years ago
Submitted
Optimal Relative Coplanar Transfer in the Orbit
Program for optimizing the control (specific thrust) for relative coplanar transfer in the orbit
7 years ago | 3 downloads |
Submitted
Implementation of Time Optimal Control Law
Implementation of time optimal control law (bang-bang controller) for a double integral system
7 years ago | 4 downloads |
