A sliding mode controller for aircraft simulated entry into spin

In this paper, two controllers are presented for commanded departure of an aircraft into spin. The first controller is designed based on the information obtained from the bifurcation analysis results of the aircraft model and trial and error simulation experiments. The second controller is a nonline...

Full description

Saved in:
Bibliographic Details
Main Authors: Rao, D. M. K. K. Venkateswara., Sinha, Nandan Kumar.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2013
Online Access:https://hdl.handle.net/10356/107141
http://hdl.handle.net/10220/17829
http://dx.doi.org/10.1016/j.ast.2012.10.011
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English
Be the first to leave a comment!
You must be logged in first