Modelling and controller design for tilt quadplane
Tilt rotor quadplane is a relatively new concept for the world which empowers the fixed wing vehicle with the Vertical Take-Off and Landing capability. VTOL will not only help remove the dependency of the aircraft on a runway but will also prove to be economically beneficial for the companies by pro...
Saved in:
Main Author: | Raj, Raunak |
---|---|
Other Authors: | Basman Elhadidi |
Format: | Theses and Dissertations |
Language: | English |
Published: |
2018
|
Subjects: | |
Online Access: | http://hdl.handle.net/10356/76233 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Nonlinear modelling and control of a quadplane
by: Sheikh Moheed Muzaffar
Published: (2018) -
Accounting for aerodynamic Interference effects for a quadplane in transition flight
by: Shahriar, Fahim
Published: (2019) -
In-flight simulation of tilt-rotor VTOL UAV using open loop wind tunnel
by: Wong, Amos Timothy Jun Han
Published: (2022) -
3-D Formulation of Formation Flight Based on Model Predictive Control with Collision Avoidance Scheme
by: Zhao, Weihua., et al.
Published: (2011) -
Design and development of a flight demonstrator
by: Sim, Yinxiang.
Published: (2009)