Back to Search
Start Over
Modeling and control of unmanned aerial/underwater vehicles using hybrid control
- Source :
- Control Engineering Practice. 76:112-122
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- Modeling and control of a multi-medium unmanned vehicle capable of seamless operation in air or underwater is introduced in this paper. The multi-medium system is treated as a hybrid system with continuous dynamics while performing in both air and underwater, and discrete jumps in the medium density during the transitions. The continuous dynamics are modeled by the Newton–Euler formalism, taking into account the effects of the buoyancy and drag phenomena, normally neglected in aerial vehicles. A hybrid controller is designed for trajectory tracking considering the full system, including a transition strategy to assure the switching between mediums. Stability analysis for the full system is provided using hybrid Lyapunov and invariance principles. The performance of the control strategy is validated through simulations. Finally, an experimental platform consisting of a multirotor in an octo-quadcopter configuration was developed and some preliminary experimental results are introduced, showing the vehicle performing in air, underwater and through the transition.
- Subjects :
- Lyapunov function
0209 industrial biotechnology
Buoyancy
Computer science
Applied Mathematics
020208 electrical & electronic engineering
02 engineering and technology
Medium density
engineering.material
Computer Science Applications
Computer Science::Robotics
symbols.namesake
Formalism (philosophy of mathematics)
020901 industrial engineering & automation
Control and Systems Engineering
Control theory
Drag
Hybrid system
0202 electrical engineering, electronic engineering, information engineering
symbols
engineering
Electrical and Electronic Engineering
Underwater
Multirotor
Subjects
Details
- ISSN :
- 09670661
- Volume :
- 76
- Database :
- OpenAIRE
- Journal :
- Control Engineering Practice
- Accession number :
- edsair.doi...........063baf4ea2ff7481458cbf63c47d9fbb