Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
An almost disturbance decoupling solution of the attitude control problem
Date
2008-01-01
Author
Doruk, R. Oezguer
Kocaoglan, Erol
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
173
views
0
downloads
Cite This
Purpose - The purpose of this paper is to derive a robust nonlinear attitude control law intended for practical application.
Subject Keywords
Systems and control theory
,
Space technology
,
Artificial satellites
URI
https://hdl.handle.net/11511/64732
Journal
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
DOI
https://doi.org/10.1108/00022660810873728
Collections
Department of Electrical and Electronics Engineering, Article
Suggestions
OpenMETU
Core
Linearization in satellite attitude control with modified Rodriguez parameters
Doruk, R. Özgür (2009-01-01)
Purpose - The purpose of this paper is to analyze the results of the Jacobian matrix linearization of the satellite attitude dynamics with modified Rodriguez parameters (MRP) as attitude representation.
Linearization-based attitude error regulation: multiplicative error case
Doruk, R. Ozgur (2009-01-01)
Purpose - The purpose of this paper is to design and simulate a linearized attitude stabilizer based on linear quadratic regulator theory (LQR) using the multiplicative definition of the attitude.
An Efficient Formula Synthesis Method with Past Signal Temporal Logic
Ergurtuna, Mert; Aydın Göl, Ebru (2019-01-01)
In this work, we propose a novel method to find temporal properties that lead to the unexpected behaviors from labeled dataset. We express these properties in past time Signal Temporal Logic (ptSTL). First, we present a novel approach for finding parameters of a template ptSTL formula, which extends the results on monotonicity based parameter synthesis. The proposed method optimizes a given monotone criteria while bounding an error. Then, we employ the parameter synthesis method in an iterative unguided for...
A complete axiomatization for fuzzy functional and multivalued dependencies in fuzzy database relations
Sozat, MI; Yazıcı, Adnan (Elsevier BV, 2001-01-15)
This paper first introduces the formal definitions of fuzzy functional and multivalued dependencies which are given on the basis of the conformance values presented here. Second, the inference rules are listed after both fuzzy functional and multivalued dependencies are shown to be consistent, that is, they reduce to those of the classic functional and multivalued dependencies when crisp attributes are involved. Finally, the inference rules presented here are shown to be sound and complete for the family of...
Using constrained intuitionistic linear logic for hybrid robotic planning problems
Saranlı, Uluç (2007-04-14)
Synthesis of robot behaviors towards nontrivial goals often requires reasoning about both discrete and continuous aspects of the underlying domain. Existing approaches in building automated tools for such synthesis problems attempt to augment methods from either discrete planning or continuous control with hybrid elements, but largely fail to ensure a uniform treatment of both aspects of the domain. In this paper, we present a new formalism, Constrained Intuitionistic Linear Logic (CILL), merging continuous...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
R. O. Doruk and E. Kocaoglan, “An almost disturbance decoupling solution of the attitude control problem,”
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
, pp. 295–307, 2008, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/64732.