Rocket Lander Dynamics Transformation in MATLAB -- 2
Budget: $10 – $30 USD
I need assistance with a MATLAB project involving a rocket lander.
The lander launches vertically, flies horizontally and lands vertically. It is controlled by engine gymbal angles in two directions, RCS for roll, and thrust variatiob.
The rocket flight is designed now integrating wrt time rotational and translational body frame dynamic equations. To get absolute ref system position and angles, so the trajectory, frame rotations are applied. The task is to transform the dynamic equations from a body reference system to an absolute system before integration.
Provided scripts as solution must verify vertical launch and descent/landing, horizontal flight and flight at an angle.
Key Requirements:
- Proficiency in MATLAB
- Strong understanding of dynamic equations
- Experience with both translational and rotational dynamics
- Ability to create and run simulations
Please provide your bid if you have the necessary skills and experience. I'm looking forward to your proposals.
The lander launches vertically, flies horizontally and lands vertically. It is controlled by engine gymbal angles in two directions, RCS for roll, and thrust variatiob.
The rocket flight is designed now integrating wrt time rotational and translational body frame dynamic equations. To get absolute ref system position and angles, so the trajectory, frame rotations are applied. The task is to transform the dynamic equations from a body reference system to an absolute system before integration.
Provided scripts as solution must verify vertical launch and descent/landing, horizontal flight and flight at an angle.
Key Requirements:
- Proficiency in MATLAB
- Strong understanding of dynamic equations
- Experience with both translational and rotational dynamics
- Ability to create and run simulations
Please provide your bid if you have the necessary skills and experience. I'm looking forward to your proposals.