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
Imaging-based attitude determination algorithm for small satellites: Design and the preliminary results
Date
2020-01-01
Author
Güzel, Mehmet Burak
Söken, Halil Ersin
Tekinalp, Ozan
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
189
views
0
downloads
Cite This
Limitations for small satellite missions encourages researchers and engineers to use on-board equipment for multiple tasks. Thus, both space can be saved and the equipment redundancy can be prevented. For Earth-imaging satellites a prominent equipment that can be used for multiple purposes is the camera. Other than the observation, the taken images can be used as measurements for determining the absolute or relative attitude of the spacecraft. Depending on also the content of the image (e.g. stars, Earth, Moon) a camera can be an alternate attitude sensor that is capable of providing high accuracy attitude measurements in low cost. This research aims at designing an attitude estimation algorithm, which can aid the coarse attitude estimates with the attitude information extracted from Earth images. Whenever an image is available to be used for attitude estimation, reference Earth data is matched with the ellipsoid that Earth image forms on the sensor frame to estimate the three-axis attitude of the spacecraft. This estimated attitude is fed to a multiplicative extended Kalman filter (MEKF) algorithm that runs as the main block of the attitude estimator. The measurements from the conventional attitude sensor block, which is formed of a three-axis magnetometer and Sun sensor, are pre-processed with QUEST algorithm to unify the measurement update process of the filter. This paper introduces the architecture of the proposed algorithm together with the details on possible methods to extract the attitude information from the obtained Earth images. Preliminary results to demonstrate the success of the algorithm are presented.
URI
https://hdl.handle.net/11511/93473
Conference Name
71st International Astronautical Congress, IAC 2020
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Design of a vision-based three-axis attitude estimation algorithm for small satellites
Güzel, Mehmet Burak; Tekinalp, Ozan; Söken, Halil Ersin; Department of Aerospace Engineering (2021-2-8)
Equipment and budget limitations of satellite missions encourages researchers to use on-board equipment for multiple tasks. Camera stands out as an ideal equipment that can be used for multiple purposes in satellites making Earth observation. In this thesis, an attitude estimation algorithm is designed to aid the coarse attitude estimates with the attitude information obtained from Earth images. Attitude information is extracted from Earth images according to perspective geometry laws. This estimated attitu...
Vision-Based Detection and Distance Estimation of Micro Unmanned Aerial Vehicles
Gökçe, Fatih; Üçoluk, Göktürk; Şahin, Erol; Kalkan, Sinan (MDPI, ST ALBAN-ANLAGE 66, CH-4052 BASEL, SWITZERLAND, 2015-9)
Detection and distance estimation of micro unmanned aerial vehicles (mUAVs) is crucial for (i) the detection of intruder mUAVs in protected environments; (ii) sense and avoid purposes on mUAVs or on other aerial vehicles and (iii) multi-mUAV control scenarios, such as environmental monitoring, surveillance and exploration. In this article, we evaluate vision algorithms as alternatives for detection and distance estimation of mUAVs, since other sensing modalities entail certain limitations on the environment...
Numerical simulation of two-dimensional collisionless plasma flows under the effect of electrostatic forces via particle in cell method
Tümüklü, Özgür; Çelenligil, Mehmet Cevdet; Şengil, Nevsan; Department of Aerospace Engineering (2013)
Taking its name from its ability to generate thrust via electricity, the concept of electric propulsion has important space mission applications like station keeping for satellites and deep space probe. However, contamination of plumes in electric propulsion systems with ion beam could hinder communication, and effective neutralization is essential to clear away this predicament. Today, computer simulation is regarded as a powerful tool to investigate plasma behavior in the plumes of electric propulsion dev...
Transfer Learning-Based Crack Detection by AutonomousUAVs
Küçüksubaşı, Fatih; Sorguç, Arzu (2018-07-20)
Unmanned Aerial Vehicles (UAVs) have recently shown great performance collecting visual data through autonomous exploration and mapping in building inspection. Yet, the number of studies is limited considering the post processing of the data and its integration with autonomous UAVs. These will enable huge steps onward into full automation of building inspection. In this regard, this work presents a decision making tool for revisiting tasks in visual building inspection by autonomous UAVs. The tool is an imp...
Design, simulation, and fabrication of cubesat antenna systems
Dolapçı, Türker; Ergül, Özgür Salih; Department of Electrical and Electronics Engineering (2020-9)
This study aims to design, simulate, and fabricate on-board and ground station antenna systems for CubeSats, i.e., the most affordable space missions. An on-board UHF turnstile antenna system is optimized in simulation evironment in accordance with different pattern requirements, by changing the orientation of the antenna arms. In order to feed the turnstile antenna arms by successive 90◦ phase differences between them, a four-way quadrature splitter circuit is designed and fabricated. Antenna pattern m...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
M. B. Güzel, H. E. Söken, and O. Tekinalp, “Imaging-based attitude determination algorithm for small satellites: Design and the preliminary results,” Virtual, Online, 2020, vol. 2020-October, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/93473.