2020
DOI: 10.1016/j.ast.2019.105549
|View full text |Cite
|
Sign up to set email alerts
|

Adaptive control for multi-rotor UAVs autonomous ship landing with mission planning

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
15
0
1

Year Published

2020
2020
2024
2024

Publication Types

Select...
7
2

Relationship

0
9

Authors

Journals

citations
Cited by 46 publications
(16 citation statements)
references
References 31 publications
0
15
0
1
Order By: Relevance
“…UAV (Unmanned Aircraft Vehicle) jenis quadrotor merupakan salah satu jenis pesawat tanpa awak yang banyak dikembangkan. Jenis pesawat ini banyak digunakan baik di kalangan militer maupun sipil karena kemudahannya dalam melakukan take-off dan landing di tempat dengan luas sangat terbatas [1]. UAV ini dapat menggunakan sistem kendali jauh (remote) atau autonomous.…”
Section: Pendahuluanunclassified
“…UAV (Unmanned Aircraft Vehicle) jenis quadrotor merupakan salah satu jenis pesawat tanpa awak yang banyak dikembangkan. Jenis pesawat ini banyak digunakan baik di kalangan militer maupun sipil karena kemudahannya dalam melakukan take-off dan landing di tempat dengan luas sangat terbatas [1]. UAV ini dapat menggunakan sistem kendali jauh (remote) atau autonomous.…”
Section: Pendahuluanunclassified
“…always holds. According to ( 25), (28), and m > 0, we can obtain u 0 and T > 0 instead of T ≥ 0, thus the singularity of the thrust force T can be avoided and the singularity of the desired attitude σ d is also avoided from (27).…”
Section: Design the Control Inputmentioning
confidence: 99%
“…An invariant ellipsoid-based method for the controller design and gain synthesis of a lowcost quadrotor autonomous landing system subjected to wind disturbance and measurement noise was proposed by [23]- [25]. Then, a class of relative motion model was developed for the shipboard landing missions by [26]- [28], and the adaptive nonlinear controllers were presented to ensure the success of the helicopter landing on the deck in rough sea. However, the dynamic couplings between the relative position and relative attitude motions were ignored, while the under-actuated property of the aeronautical vehicles was also insufficiently considered in the previous works.…”
Section: Introductionmentioning
confidence: 99%
“…In order to avoid collision, an effective solution is to utilize a ship motion predictor. With the predicted information, the landing phase will be switched on only when there would be a future period in which the ship's pitch and roll remain small values [4]. Thus, the necessary controlled states are reduced to 4 DOF including relative position and relative yaw.…”
Section: Introductionmentioning
confidence: 99%