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Proportional-derivative linear quadratic regulator controller design for improved longitudinal motion control of unmanned aerial vehicles
- Source :
- International Journal of Micro Air Vehicles. 8:41-50
- Publication Year :
- 2016
- Publisher :
- SAGE Publications, 2016.
-
Abstract
- This study investigates the longitudinal motion control of unmanned aerial vehicles through a simulation in MATLAB. The linear model of an unmanned aerial vehicle is applied to controllers to explicate the longitudinal motion of the unmanned aerial vehicle. The ideal performance for an unmanned aerial vehicle is to achieve the desired response instantly with 100% precision. However, currently available controllers need further improvements. Thus, a proportional-derivative linear quadratic regulator controller is developed and compared with a proportional-integral-derivative controller, a linear quadratic regulator controller, and a proportional linear quadratic regulator controller. The proportional-derivative linear quadratic regulator controller enhances the response of the system by reducing settling time by more than 95% compared with other available controllers. Additionally, the proportional-derivative linear quadratic regulator improves the root mean square error by almost 50% compared with the proportional linear quadratic regulator controller and improves rise time by almost 96% with reasonable overshoot.
- Subjects :
- 0209 industrial biotechnology
Computer science
Settling time
Linear model
Aerospace Engineering
PID controller
Control engineering
02 engineering and technology
Linear-quadratic regulator
Motion control
020901 industrial engineering & automation
Control theory
0202 electrical engineering, electronic engineering, information engineering
Overshoot (signal)
020201 artificial intelligence & image processing
Micro air vehicle
MATLAB
computer
computer.programming_language
Subjects
Details
- ISSN :
- 17568307 and 17568293
- Volume :
- 8
- Database :
- OpenAIRE
- Journal :
- International Journal of Micro Air Vehicles
- Accession number :
- edsair.doi...........96b5cc993e4000d6676e09b101c3af1a