2021
DOI: 10.3390/en14082292
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Adaptive Control and Estimation of the Condition of a Small Unmanned Aircraft Using a Kalman Filter

Abstract: The article was motivated by the design of adaptive control algorithms for the control of a a fixed wing unmanned aerial vehicle (UAV). An adaptive system is a system that, with its structure or parameters, adapts to changes in the behavior of the object and based on the knowledge of variable properties, maintains the quality of its regulatory transition. The knowledge gained on this small UAV can be applied to larger aircraft. The creation of the proposed adaptive control into the UAV consisted of the creatio… Show more

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Cited by 5 publications
(6 citation statements)
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“…If, in moving in the previous relation ( 5) N(t) to the left and dividing both parts of it by 𝑁 . ∆𝑡, we obtain [15,20]:…”
Section: Unmanned Aerial Vehicle Readiness For Local Flight In a Moun...mentioning
confidence: 99%
See 4 more Smart Citations
“…If, in moving in the previous relation ( 5) N(t) to the left and dividing both parts of it by 𝑁 . ∆𝑡, we obtain [15,20]:…”
Section: Unmanned Aerial Vehicle Readiness For Local Flight In a Moun...mentioning
confidence: 99%
“…where ∆m(t + ∆t) is the number of signal loss recovery (GPS) activities per time ∆t and ∆n(t + ∆t) is the number of malfunctioning systems with a given UAV error. If, in moving in the previous relation ( 5) N(t) to the left and dividing both parts of it by N o .∆t, we obtain [15,20]:…”
Section: Unmanned Aerial Vehicle Readiness For Local Flight In a Moun...mentioning
confidence: 99%
See 3 more Smart Citations