TY - GEN
T1 - Payload Delivery through Acrobatic Quadrotor Flip-and-Throw Maneuver Using Model Predictive Control
AU - Jain, Saransh
AU - Shethwala, Yash
AU - Akurathi, Swaraj
AU - Das, Jnaneshwar
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - This paper presents a novel approach for delivering payloads using quadrotor drones, by leveraging acrobatic flip or 'belly-flop' maneuver. This method not only leverages the agility of quadrotors but also offers a practical solution for deploying sensor probes into inaccessible or hazardous areas, such as volcanic vents, without the need for additional mechanical devices such as spring-based or compressed-air projectile launchers. By employing Model Predictive Control (MPC), our methodology enables real-time trajectory planning and precise execution of flip maneuvers, taking into account the dynamics of the quadrotor, payload, rotors, and thrusters. This approach ensures stable and dynamic flights even during aggressive maneuvers. The effectiveness of our method has been tested through simulations in ROS and Gazebo environments, as well as real-world experiments conducted at the ASU Drone Studio using a low-SWaP-C agile quadrotor drone equipped with a Pixhawk flight controller and an Odroid M1 companion computer. These tests demonstrated the feasibility of flip-and-throw maneuvers for payload delivery and highlighted the system's accuracy in trajectory tracking and response times. The findings from this research can advance autonomous aerial robotics in tasks requiring high precision and agility, such as delivering probes into inaccessible zones and optimizing image capture angles through acrobatic flight paths.
AB - This paper presents a novel approach for delivering payloads using quadrotor drones, by leveraging acrobatic flip or 'belly-flop' maneuver. This method not only leverages the agility of quadrotors but also offers a practical solution for deploying sensor probes into inaccessible or hazardous areas, such as volcanic vents, without the need for additional mechanical devices such as spring-based or compressed-air projectile launchers. By employing Model Predictive Control (MPC), our methodology enables real-time trajectory planning and precise execution of flip maneuvers, taking into account the dynamics of the quadrotor, payload, rotors, and thrusters. This approach ensures stable and dynamic flights even during aggressive maneuvers. The effectiveness of our method has been tested through simulations in ROS and Gazebo environments, as well as real-world experiments conducted at the ASU Drone Studio using a low-SWaP-C agile quadrotor drone equipped with a Pixhawk flight controller and an Odroid M1 companion computer. These tests demonstrated the feasibility of flip-and-throw maneuvers for payload delivery and highlighted the system's accuracy in trajectory tracking and response times. The findings from this research can advance autonomous aerial robotics in tasks requiring high precision and agility, such as delivering probes into inaccessible zones and optimizing image capture angles through acrobatic flight paths.
UR - https://www.scopus.com/pages/publications/85208259570
UR - https://www.scopus.com/pages/publications/85208259570#tab=citedBy
U2 - 10.1109/CASE59546.2024.10711775
DO - 10.1109/CASE59546.2024.10711775
M3 - Conference contribution
AN - SCOPUS:85208259570
T3 - IEEE International Conference on Automation Science and Engineering
SP - 2463
EP - 2470
BT - 2024 IEEE 20th International Conference on Automation Science and Engineering, CASE 2024
PB - IEEE Computer Society
T2 - 20th IEEE International Conference on Automation Science and Engineering, CASE 2024
Y2 - 28 August 2024 through 1 September 2024
ER -