Orbit Design and Simulation for Kufasat Nanosatellite
Open accessAbstract
Orbit design for KufaSat Nano-satellites is presented. Polar orbit is selected for the KufaSat mission. The orbit was designed with an Inclination which enables the satellite to see every part of the earth. KufaSat has a payload for imaging purposes which require a large amount of power, so the orbit is determined to be sun synchronous in order to provide the power through solar panels. The KufaSat mission is designed for the low earth orbit. The six initial Keplerian Elements of KufaSat are calculated. The orbit design of KufaSat according to the calculated Keplerian elements has been simulated and analyzed by using MATLAB first and then by using General Mission Analysis Tool.
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Research works printed but not linked: 6
- Afful M. A., 2013 "Orbital Lifetime Predictions of Low Earth Orbit Satellites and the effect of a DeOrbitSail", Master Thesis, Stellenbosch University.
- Chessab M. M., 2013, "Gravity Gradient Stabilization of Nano Satellite Using Fuzzy Logic Controller", Master Thesis University of Kufa.
- Chessab M. M., Shehab Abd-AL-Razak, 2014, "Direct Fuzzy Logic Controller for Nano- Satellite", Journal of Control Engineering and Technology JCET, Vol. 4 Issue. 3. DOI: 10.14511/jcet. · DOI
- Chobotov V. A. 2002, Orbital Mechanics Third Edition, AIAA Education Series.
- Eshagh M. and N. Alamdari, 2007, "Perturbations in orbital elements of a low earth orbiting satellite", Journal of the Earth & Space Physics. Vol. 33, No. 1, P. 1-12.
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- Authors
- Mahdi, M. C.
- Affiliations
- Al-Furat Al-Awsat Technical University (IQ)
- Corresponding author
- Mahdi, Mohammed Chessab
- Venue
- Artificial Satellites
- Publisher
- Walter de Gruyter GmbH
- Published
- 2015-12-01
- Volume
- 50
- Issue
- 4
- Pages
- 157-168
- ISSN
- 0208-841X (ISSN-L)
- 2083-6104
- OpenAlex
- W2334716014
- Cited by
- 7
- References
- 0
- Citations by year
- 2022: 1 · 2021: 1 · 2020: 1 · 2019: 1 · 2018: 2 · 2016: 1
- FWCI
- 1.45
- Type
- journal article
- Language
- en
- Open access
- hybrid
- doi.org
- Locations
- Artificial Satellites (publishedVersion, cc-by)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
- Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
- Keywords
- nanosatellites, orbit design, polar orbit, sun-synchronous orbit, orbital elements, low Earth orbit, solar energy, satellite imaging, orbit simulation
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