Abstract
A substantial interest in aerial robots has grown in recent years. However, the energetic cost of flying is one of the key challenges nowadays. Rotorcrafts are heavier-than-air flying machines that use lift generated by one or several rotors (vertically oriented propellers), and because of this, they spend a large proportion of their available energy to maintain their own weight in the air. In this brief, this concept is used to evaluate the relationship between navigation speed and energy consumption in a miniature quadrotor helicopter, which travels over a desired path. A novel path-following controller is proposed in which the speed of the rotorcraft is a dynamic profile that varies with the geometric requirements of the desired path. The stability of the control law is proved using the Lyapunov theory. The experimental results using a real quadrotor show the good performance of the proposed controller, and the percentages of involved energy are quantified using a model of a lithium polymer battery that was previously identified.
| Original language | English |
|---|---|
| Pages (from-to) | 1423-1430 |
| Number of pages | 8 |
| Journal | IEEE Transactions on Control Systems Technology |
| Volume | 25 |
| Issue number | 4 |
| DOIs | |
| Publication status | Published - 1 Jul 2017 |
Bibliographical note
Publisher Copyright:© 1993-2012 IEEE.
Keywords
- Energy consumption
- kinematic model
- path-following controller
- quadrotor
- unmanned aerial vehicles (UAVs)
