Spacecraft Trajectory Design and Optimization
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Astronautics & Space Science".
Deadline for manuscript submissions: closed (15 September 2021) | Viewed by 11076
Special Issue Editor
Special Issue Information
Dear Colleagues,
Space has been one of the fields that has attracted public attention for the past few years. Various space missions have been executed or proposed, such as lunar missions, interplanetary missions, asteroid missions, small/cubic satellite missions, debris removal, space situational awareness, and so on. The success of these missions highly relies on trajectory design, navigation, guidance, and control. For small-sized spacecrafts, such as micro-satellites or CubeSats, optimization of trajectory control is even crucial. Novel algorithms and newly developed tools such as artificial intelligence have greatly increased capacities and brought innovated the field. Development, however, brings with it challenging problems to solve.
This Special Issue focuses on the recent advances and novel algorithms of spacecraft-trajectory-related research. Research on the trajectory of small-sized probes or on deep space exploration is encouraged. Authors are invited to submit full research articles and review manuscripts addressing (but not limited to) the following topics:
- Spacecraft trajectory design in deep space missions;
- Navigation, guidance and control of spacecraft trajectory;
- Optimization of spacecraft trajectory control;
- Application of AI to spacecraft trajectory;
- Trajectory design and control of small-sized spacecraft;
- Space situation awareness;
- Continuous low-thrust trajectory;
- Spacecraft trajectory with novel propulsion system;
- Formation flight.
Prof. Fu-yuen Hsiao
Guest Editor
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 2400 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.
Keywords
- Spacecraft trajectory design
- Navigation, guidance, and control of spacecraft trajectory
- Spacecraft trajectory optimization
- Artificial intelligence in spacecraft trajectory
- Deep space missions
- Novel algorithms