2023
DOI: 10.3390/drones7030201
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Control Architecture for a Quadrotor Transporting a Cable-Suspended Load of Uncertain Mass

Abstract: This paper presents an architecture for controlling a quadrotor transporting a cable-suspended load of uncertain mass. A family of trajectories is proposed that is composed by three phases—lift-off, transit, and landing—and implemented as a hybrid system. The proposed control system uses an adaptive geometric controller with asymptotic tracking stability. The mass of the transported load was estimated using an adaptive mechanism, which adjusts the action resorting to a geometric control method. The resulting s… Show more

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Cited by 5 publications
(4 citation statements)
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“…When validation is indoors, wind is proven not to be the most relevant disturbance, but most researchers work with unknown payload masses or variations in the planned path. Some examples of these disturbances are in [107,114,144].…”
Section: Trends In Technologymentioning
confidence: 99%
See 1 more Smart Citation
“…When validation is indoors, wind is proven not to be the most relevant disturbance, but most researchers work with unknown payload masses or variations in the planned path. Some examples of these disturbances are in [107,114,144].…”
Section: Trends In Technologymentioning
confidence: 99%
“…Particularly in multi-UAV systems, more real experimentation is required. References:[39,40,46,48,50,51,53,89,144] Flexible cable Flexible cables enhance some dynamic properties in simulations. The most used models are the spring-and-damping model and the cable formed by a series of weighted extensible segments of different sizes, connected with spherical joints.…”
mentioning
confidence: 99%
“…The quadrotor suspension system is a versatile technology with diverse applications [1,2], including freight transport [3][4][5][6], agriculture, forestry, crop protection, and environmental sensing [7]. This system is highly regarded for its exceptional flight flexibility, cost effectiveness, and ease of loading and unloading [8][9][10][11].…”
Section: Introductionmentioning
confidence: 99%
“…The problem of a single rotorcraft carrying a load has been addressed in the literature considering minimal load swing, with a number of works investigating different control approaches [5][6][7][8][9][10][11][12][13][14][15][16][17][18]. In [16], for example, the transportation problem is solved by an energy-based control strategy and a nonlinear feedback controller based on Linear Matrix Inequality (LMI).…”
Section: Introductionmentioning
confidence: 99%