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
Development of a flexible satellite simulator and associated control algorithms.
Download
119302.pdf
Date
2002
Author
Taylan, Koray
Metadata
Show full item record
Item Usage Stats
82
views
0
downloads
Cite This
URI
https://hdl.handle.net/11511/12860
Collections
Graduate School of Natural and Applied Sciences, Thesis
Suggestions
OpenMETU
Core
Development of a PC-based partial discharge detection and measurement system.
Taşcı, Alper; Hızal, Mirzahan; Department of Electrical and Electronics Engineering (2002)
Development of a digital computer program for the simulation of A 4-Stroke direct injection diesel engine cycle.
Ali, Ibrahim; Department of Mechanical Engineering (1980)
Development of a digital computer program for the simulation of the powwer cycle and pollutant formation in spark ignited engines.
Nişli, Serdar; Department of Mechanical Engineering (1982)
Development of a conceptual design tool and calculation of stability and control derivatives for mini UAV systems
Yazırlı, Sena; Alemdaroğlu, Hüseyin Nafiz; Department of Aerospace Engineering (2015)
The main objective of this thesis is to write a design tool that will perform the conceptual design phase of an aircraft and achieve the desired specifications of the design. For this purpose, a code is written in MATLAB so that the designer does not have to change or check parameter values when a modification on the mission altitude, cruise conditions, airfoil type, propulsion system units, weight or general geometry of the aircraft. Most of the available design tools are created for large aircraft and not...
Development of an octree based grid coarsening and multigrid flow solution
Mahmutyazıcıoğlu, Emel; Aksel, Mehmet Haluk; Tuncer, İsmail Hakkı; Department of Mechanical Engineering (2010)
The multigrid technique is one of the most effective techniques to achieve the reduction of the CPU cost for flow solvers. The multigrid strategy uses the multilevel grids which are the coarsening subsets of fine grid. An explicit solver rapidly reduces the high frequency errors on the computational grids. Since high frequency errors on coarse grids correspond to low frequency errors on fine grids, cycling through the coarse grid levels rapidly reduces the errors ranging from high-to-low frequency. The aim ...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
K. Taylan, “Development of a flexible satellite simulator and associated control algorithms.,” Middle East Technical University, 2002.