Optimization of space orbits design for Earth orbiting missions

O Abdelkhalik, A Gad - Acta Astronautica, 2011 - Elsevier
In Earth orbiting space missions, the orbit selection dictates the mission parameters like the
ground resolution, the area coverage, and the frequency of coverage parameters. To …

Multiobjective optimization in repeating sun-synchronous orbits design for remote-sensing satellites

B Saboori, AM Bidgoli, B Saboori - Journal of Aerospace …, 2014 - ascelibrary.org
Orbit design is a very important and fundamental task in the mission analysis and design of
a satellite. In the present paper, a multiobjective optimization tool is developed for the …

Sun-synchronous repeat ground tracks and other useful orbits for future space missions

SW Paek, S Kim, L Kronig, O de Weck - The Aeronautical Journal, 2020 - cambridge.org
The development of oceanography and meteorology has greatly benefited from satellite-
based data of Earth's atmosphere and ocean. Traditional Earth observation missions have …

[HTML][HTML] A framework for developing an attitude determination and control system simulator for Cubesats: Processor-in-loop testing approach

M Haloua, Z Guennoun, Z Moudden - Results in Engineering, 2024 - Elsevier
The outbreak of miniaturized satellites is increasingly demanding well-performing attitude
determination and control systems (ADCS). Testing an ADCS directly using hardware is …

Two-way orbits

O Abdelkhalik, D Mortari - Celestial Mechanics and Dynamical Astronomy, 2006 - Springer
This paper introduces a new set of compatible orbits called “Two-Way Orbits,” whose ground
track path is a closed-loop trajectory that intersects at certain points with tangent …

Electromagnetic Characterization of the Ionosphere in the Framework of the Magnetosphere-Ionosphere-Lithosphere Coupling

D Recchiuti - 2024 - iris.unitn.it
The ionospheric environment has become a focal point in the study of earthquake-related
anomalies. In particular, both electromagnetic anomalies and particle bursts have been …

[图书][B] Evaluating Solar Array Positioning Designs for Small Satellites in Different Orbits

MAA Mohamed - 2023 - search.proquest.com
Access to space has consistently presented difficulties, particularly for universities and
research with limited financial resources. Overcoming high costs, long development times …

Repeated Shadow Track Orbits for Space‐SunSetter Missions

A Gad, O Abdelkhalik - International Journal of Aerospace …, 2009 - Wiley Online Library
This paper introduces a new set of orbits, the “Repeated Shadow Track Orbits.” In these
orbits, the shadow of a spacecraft on the Earth visits the same locations periodically every …

Preliminary Mission Analysis and Sub-System Design for the 16U4SBSP CubeSat Mission

C Busso - 2024 - webthesis.biblio.polito.it
The mission concept “16U4SBSP”, funded by the European Space Agency through the
Sysnova campaign “Innovative Missions Concepts enabled by Swarms of Cube-Sats”, aims …

[PDF][PDF] Correction Maneuver Optimization to Maintain The Local Time of Lapan-A4 Satellite

MR Zuhri, RE Poetro, T Indriyanto… - Indonesian Journal of …, 2023 - ejournal.brin.go.id
In order for a satellite to achieve a sun-synchronous orbit (SSO), it must have a nodal
precession rate equal to the revolution rate of the Earth around the Sun. However, sun …