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

180
views

0
downloads

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

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.