Estimation of states for autonomous fixed wing aircraft

Highlights 🔗

• Equations are derived for EKF using dynamics of fixed wing aircraft
• Equations are verified using MATLAB and Simulink simulations for the scenarios of takeoff, cruise and landing
• Algorithm implemented in Python/C++, ROS and tested in Gazebo environment

Problem Statement 🔗

• Aim is to estimate states of the autonomous fixed wing aircraft

Ideation 🔗

Solution Methodology 🔗

Results and Conclusion 🔗