2021
DOI: 10.1166/jno.2021.2996
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Flight Control System Design and Autonomous Flight Control of Small-Scale Unmanned Helicopter Based on Nanosensors

Abstract: Due to the limitation of the size and power, micro unmanned aerial vehicle (MUAV) usually has a small load capacity. Aiming at the problems of limited installation space and easy being interfered in flight attitude measurement of the small-scale unmanned helicopter (SUH), a low-cost and lightweight flight control system of the SUH based on ARM Cortex-M4 core microcontroller and Micro-Electro-Mechanical Systems (MEMS) sensors is developed in this paper. On this basis, in order to realize the autonomous flight … Show more

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Cited by 4 publications
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“…Thus, UAVs are suitable for dangerous missions, such as reconnaissance, rescue, and operation missions. Compared with fixed-wing UAVs, unmanned aerial helicopters (UAHs) have the ability to hover [4][5][6][7]. Due to this, combined with their lower detectability, unmanned helicopters are more suitable for low-altitude stealth missions, such as close air support and specific target raids.…”
Section: Introductionmentioning
confidence: 99%
“…Thus, UAVs are suitable for dangerous missions, such as reconnaissance, rescue, and operation missions. Compared with fixed-wing UAVs, unmanned aerial helicopters (UAHs) have the ability to hover [4][5][6][7]. Due to this, combined with their lower detectability, unmanned helicopters are more suitable for low-altitude stealth missions, such as close air support and specific target raids.…”
Section: Introductionmentioning
confidence: 99%