Special Issue "Orbit Determination of Earth Orbiting Objects"
A special issue of Aerospace (ISSN 2226-4310).
Deadline for manuscript submissions: closed (31 August 2020) | Viewed by 2976
Interests: space; satellite; astrodynamics; control systems engineering; space technology; spacecraft; aeronautical engineering; orbital mechanics
The development of emerging technologies aiming to reduce the size of electronic components, thus improving their efficiency, give a dramatic impulse to launch a large number of objects into orbit. The number of nano- and micro-satellites, as well as CubeSats, are increasing constantly, and new mega constellations will overcrowd the Earth’s orbit in the near future. This situation will lead to needing more efficient and reliable technologies for tracking and measuring orbital objects, both operative and not. For example, as the requirements in measurement accuracy for determining the impact point of the reentering objects have increased to meet the growing demands of public safety, traditional methods have to be improved, together with the introduction of more advanced analysis techniques and observation technologies. Complex systems based on ground-based measurements (radar and optical), capable of improving the accuracy of trajectory determination, and to permit the physical characterization, in terms of shape and materials, of these objects, may be expected to continuously drive advancement in this field.
This Special Issue aims to provide an overview of the recent advances in trajectory and attitude estimation, and the physical characterization of Earth orbiting objects, especially applied to the operation and reentry phase. Authors are invited to submit full research articles and review manuscripts addressing (but not limited to) the following topics:
- Methods for initial orbit determination
- Catalogue build-up and maintenance
- Data fusion from different sources
- Advanced ground- and space-based measurement techniques
- Attitude determination of orbiting objects from on ground measurements
- Photometry and spectroscopy of space debris
- Reentering object trajectory estimation
- Conjunction analysis
- Mega constellation tracking and measurements
Prof. Dr. Fabrizio Piergentili
Manuscript Submission Information
Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.
Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Aerospace is an international peer-reviewed open access monthly journal published by MDPI.
Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 1600 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.
- orbit and attitude determination
- space debris measurements