2023
DOI: 10.1088/1755-1315/1203/1/012027
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Multi-criteria Genetic Algorithm Optimization Approach for Balancing Bicopter Control

Esa Apriaskar,
Dhidik Prastiyanto,
Akhyar Abdillah Manaf
et al.

Abstract: Efforts to find the best controller for stabilizing a flying vehicle have been widely developed in recent years. This work aims to join the development track by exploring the use of genetic algorithm (GA) to find the most optimum controller parameter considering settling time and overshoot criteria. Roll attitude control of a balancing bicopter was chosen as the applied plant to confirm the designed method. The controller structure applied in this research is an ideal proportional-integral (PI) controller. Two… Show more

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Cited by 3 publications
(2 citation statements)
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“…Subsequently, equation ( 6) defines the performance index as a K matrix. The P component in equation ( 6) is a positive semidefinite solution to the Algebraic Riccati Equation (ARE) which needs to persuade as written in equation (7).…”
Section: π‘₯(𝑑) = 𝐴π‘₯(𝑑) + 𝐡𝐡(𝑑)mentioning
confidence: 99%
See 1 more Smart Citation
“…Subsequently, equation ( 6) defines the performance index as a K matrix. The P component in equation ( 6) is a positive semidefinite solution to the Algebraic Riccati Equation (ARE) which needs to persuade as written in equation (7).…”
Section: π‘₯(𝑑) = 𝐴π‘₯(𝑑) + 𝐡𝐡(𝑑)mentioning
confidence: 99%
“…This can be explained by a reduction in the number of rotors can lead to lower unit power demand, which improves flight time and saves energy [6]. However, designing a controller for a bicopter can be challenging as it needs to stabilize the bicopter, reduce settling time, and overcome oscillation simultaneously [7]. Furthermore, it is still uncommon to find control methods developed in bicopter technology, particularly those that harness the assistance of artificial intelligence (AI).…”
Section: Introductionmentioning
confidence: 99%