The main focus of this project is to design a quadcopter capable of autonomously navigating through a trajectory in 2D plane.
- Cruise control/PID Tuning
- Gain Tuning
- Stopping Distance cum deceleration calculation
- Thrust Weight Determination
- 1D Quadcopter control
- 2D Quadcopter control
The first three activities majorly focussing on intuition of control problem
- High proportional gain to reach the destination swiftly- 100
- Moderately low differential gain just enough to stop overshoot- 16
- Quadcopter designed is uniform and linear in motion/input, i.e near hover configuration
- Thrust(u1) must be high for greater acceleration in order to propel forward and reach the destination quickly
- Moment(u2) must be low to satisfy near-hover conditions
- Accordingly the quadcopter designed moves as below with no aggressive manuevers
Analysis of ideal linearized models enable better understanding and give the intuition to work with complex non-linear systems analysis and design, which is the main focus of this project.
A PD controller was designed that controls the quadcopter in 3D space in a linear fashion.