2012
DOI: 10.1007/s10846-012-9656-y
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Chaos-Genetic Algorithm for the System Identification of a Small Unmanned Helicopter

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Cited by 12 publications
(12 citation statements)
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“…During the experiment, all vehicle state variables were sampled at 50 Hz and recorded in a 4 GB flash memory on the flight control system. 27 To realize the accurate path following of UAV, even in the presence of wind disturbance, we assume that the altitude and the airspeed are maintained well. Figure 2 shows the flowchart of the proposed robust path following controller.…”
Section: System Descriptionmentioning
confidence: 99%
“…During the experiment, all vehicle state variables were sampled at 50 Hz and recorded in a 4 GB flash memory on the flight control system. 27 To realize the accurate path following of UAV, even in the presence of wind disturbance, we assume that the altitude and the airspeed are maintained well. Figure 2 shows the flowchart of the proposed robust path following controller.…”
Section: System Descriptionmentioning
confidence: 99%
“…Hence, the helicopter dynamics can be separated into two interconnected subsystems, that is, the horizontal and vertical motions. In particular, the subsystems are given by (7), which were proposed in [23] and used successfully in [24] hor = hor hor + hor hor , ver = ver ver + ver ver ,…”
Section: Helicopter Dynamical Modelmentioning
confidence: 99%
“…6 Wang et al 15 proposed a chaos genetic algorithm (GA) to identify the linear helicopter model. 6 Wang et al 15 proposed a chaos genetic algorithm (GA) to identify the linear helicopter model.…”
Section: Introductionmentioning
confidence: 99%
“…At present, the least squares and maximum likelihood methods play an important role in the development of the whole identification theory, many scholars have studied these two methods, and many improved algorithms have appeared. 6 Wang et al 15 proposed a chaos genetic algorithm (GA) to identify the linear helicopter model. Alfi 16 applied a novel particle swarm optimization (PSO), to cope with the online system parameter identification problem.…”
Section: Introductionmentioning
confidence: 99%