Altitude and Flight Speed Control System on VTOL-Plane UAVS Using the LQR Method
A VTOL-Plane UAV has a wide flight speed range. Rotary wings can only fly at very low horizontal translation speeds. Fixed-wing requires a more incredible speed than the stall speed to get enough wing lift. Combined fixed-wing and rotary-wing concepts can fly at speeds below the stall speed. The fli...
Saved in:
Main Authors: | Ashari, Ahmad, Dharmawan, Andi |
---|---|
Format: | Article PeerReviewed |
Language: | English |
Published: |
ICIC International
2022
|
Subjects: | |
Online Access: | https://repository.ugm.ac.id/282908/1/elb-13-03-01.pdf https://repository.ugm.ac.id/282908/ https://cir.nii.ac.jp/crid/1390009382722009344 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Universitas Gadjah Mada |
Language: | English |
Similar Items
-
Altitude and Flight Speed Control System on VTOL-Plane UAVS Using The LQR Method
by: Ashari, Ahmad, et al.
Published: (2022) -
Waypoint Tracking of A Fixed-Wing UAV Using The L1 Cross Track Error Control
by: Nugroho, Gesang, et al.
Published: (2022) -
Tuning LQR Parameters using Neuro Evolution of Augmenting Topologies (NEAT) on a Double Pendulum Cart
by: Fahmizal, Fahmizal, et al.
Published: (2022) -
Vertical Take-Off and Landing (VTOL) System Based On Noise Parameter for Exploring of Continuous Reinforcement Learning Approach
by: Surriani, Atikah, et al.
Published: (2022) -
Effects of rotational speed on the mechanical properties and performance of AA6061-T6 aluminium alloy in similar rotary friction welding
by: Sasmito, Agus, et al.
Published: (2023)