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
Flight Mechanics
Date
2017
Author
Yavrucuk, İlkay
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
923
views
0
downloads
Cite This
Reference frames, coordinate systems and transformations. Aircraft general equations of motion, small gain theory, longitudinal static stability and control, lateral static stability and control. Stability derivatives. Dynamic stability of uncontrolled motion.
URI
https://ocw.metu.edu.tr/course/view.php?id=261
https://hdl.handle.net/11511/36944
Collections
Department of Aerospace Engineering, Course Material
Suggestions
OpenMETU
Core
Analysis of Image Registration with Tangent Distance
Vural, Elif (2014-01-01)
The computation of the geometric transformation between a reference and a target image, known as registration or alignment, corresponds to the projection of the target image onto the transformation manifold of the reference image (the set of images generated by its geometric transformations). However, it often takes a nontrivial form such that the exact computation of projections on the manifold is difficult. The tangent distance method is an effective algorithm for solving this problem by exploiting a line...
Aerodynamic design optimization of three dimensional rocket nozzles using adjoint method
Eyi, Sinan (null; 2013-09-13)
A design optimization method based on three dimensional Euler equations is developed. A finite volume method is implemented to discretize the Euler equations. Newton's method is used to solve the discretized form of Euler equations. Newton's method requires the calculation of the Jacobian matrix which is the derivative of the residual vector with respect to the flux vector. Different upwind methods are used in the calculation of flux vectors. Numerical and analytical methods are utilized in the evaluation o...
Head modeling with camera auto-calibration and deformation
Hassanpour, R; Atalay, Mehmet Volkan (2002-01-01)
A 3D head modeling method from a sequence of 2D images is described. The views from which the input images are acquired are not calibrated., Therefore, an auto-calibration method for a sequence of images with small rotations and translation is developed. For this purpose, we have modified an already existing auto-calibration algorithm to incorporate known aspect ratio and skew values to make it applicable for small rotation around a single axis. We apply this auto-calibration technique to head (face) modeli...
Modeling Electromagnetic Scattering from Random Array of Objects by Form Invariance of Maxwell's Equations
ÖZGÜN, ÖZLEM; Kuzuoğlu, Mustafa (2015-07-24)
Electromagnetic scattering from a random array of objects is modeled by using special coordinate transformations that are based on the form invariance property of Maxwell's equations. The main motivation is to perform multiple realizations of Monte Carlo simulations corresponding to different positions of objects in an efficient way by using a single mesh. This is achieved by locating transformation media within the computational domain. The proposed approach is applied to finite element method and tested b...
Design of Compact Nano-Optical Couplers Involving Dielectric Nanorods
Karaosmanoglu, Bariscan; Yazar, Sirin; Ergül, Özgür Salih (2018-06-01)
We present optimization and design of nano-optical couplers involving dielectric nanorods. Using tens of elements, optimal array configurations are found to produce alternative responses that can be digitized. For realistic simulations, the couplers are modeled as three-dimensional structures and analyzed via surface integral equations and the multilevel fast multipole algorithm (MLFMA). Initial results are presented demonstrate the feasibility of compact but effective couplers with desired responses.
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
İ. Yavrucuk, “Flight Mechanics,” 00, 2017, Accessed: 00, 2020. [Online]. Available: https://ocw.metu.edu.tr/course/view.php?id=261.