2021
DOI: 10.1109/tnnls.2021.3080980
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Visual Navigation and Landing Control of an Unmanned Aerial Vehicle on a Moving Autonomous Surface Vehicle via Adaptive Learning

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Cited by 43 publications
(21 citation statements)
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“…The input gate structure is a gate structure that combines the state of historical information and the state of input information to perform calculations, as shown in Equations ( 8) and (9).…”
Section: ∂E ∂Kmentioning
confidence: 99%
See 1 more Smart Citation
“…The input gate structure is a gate structure that combines the state of historical information and the state of input information to perform calculations, as shown in Equations ( 8) and (9).…”
Section: ∂E ∂Kmentioning
confidence: 99%
“…With the continuous development of sensors and navigation technology, a large number of studies have been conducted on the autonomous navigation methods of quadrotor UAVs, and the development of UAVs toward autonomous navigation and flight has been promoted. Zhang et al [9] designed a multinested autonomous landing algorithm for UAV autonomous landing on unmanned surface craft ASV and conducted experimental research. At the same time, they derived a theory suitable for the stability of UAVs based on the Lyapunov stability theory and conducted experiments on the stability of UAV landings.…”
Section: Introductionmentioning
confidence: 99%
“…For the second challenge of achieving decentralization, Lee et al [13] present an interesting solution to finding a ship and its pose using classical vision algorithms. Zhang et al [14] take a different approach and present a learning-based linear controller that receives inputs from a fiducial marker to land the UAV on a USV that is subject to the waves of a lake. Furthermore, some works also present the application of an MPC controller that enables a flexible-blade helicopter to land on a marine vessel [15], [16].…”
Section: Introductionmentioning
confidence: 99%
“…1 The PALS uses a vertical rate (H-dot) reference for guidance, the inner-loop is basically a PID controller that specified with vertical rate, acceleration, and pitch rate feedback. [2][3][4] In addition, some other modern control techniques such as backstepping control, 5 sliding mode control, 6 preview control, 7 active disturbance rejection control, 8 intelligent control, 9 and visual servoing control 10 have been applied in ACLS or aircraft flight controller design.…”
Section: Introductionmentioning
confidence: 99%