Mission Analysis and Design of Lighter-than-Air Flying Vehicles (2nd Edition)
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: closed (20 June 2024) | Viewed by 8551
Special Issue Editors
Interests: electric aircraft; hybrid-electric aircraft; hydrogen-powered aircraft; aircraft preliminary design; airship; LTA; aerospace sensors and systems; aerospace instrumentation systems; UAS; flight testing
Special Issues, Collections and Topics in MDPI journals
Interests: aircraft design; electric aircraft; hybrid-electric aircraft; optimal design; aircraft modeling and simulation; airship design; wind turbine control
Special Issues, Collections and Topics in MDPI journals
Special Issue Information
Dear Colleagues,
Following the great interest shown by contributors and readers for the topics of our previous Special Issue in MDPI's Aerospace journal, we are pleased to announce a second edition devoted to novel studies related to lighter-than-air (LTA) flying vehicles. LTA vehicles are gaining the attention of the industry, thanks primarily to the improvement they offer in terms of endurance in flight and ease of operation (ground infrastructures) compared to fixed-wing aircraft and rotorcraft. Furthermore, they cope, in principle, very well with fully electric or hybrid-electric power-trains, since less energy and power should be needed with respect to other flying vehicles to fly an assigned mission.
This Special Issue aims to collect articles that present the outcomes of current research in the field of LTA vehicles, with two particular focal points: the first is on mission study, including novel possible missions for LTA vehicles, the negotiation of specifications, comparisons to other flying machines (also in terms of ground equipment), etc. This shall trace a map of the most likely missions that could potentially be covered by LTA vehicles, accounting for current technology. The second focus is on preliminary design: in principle, electrification enables some advantages, such as an increase in endurance and the achievement of novel control configurations based on thrust vectoring, but an increase in weight may result from the adoption of batteries or other electric components, thus requiring trade-off analysis to select the most promising design solutions. Developing on this focus may produce a knowledge base supporting industrial design processes.
Prof. Dr. Alberto Rolando
Prof. Dr. Carlo E. D. Riboldi
Guest Editors
Manuscript Submission Information
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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
- lighter than air
- airship
- mission design
- scenario study
- mission analysis
- balloon
- electric
- solar power
- hybrid electric
- fuel cell
- hydrogen
- helium
- electrification
- operation
- ground support
- ground infrastructure
- hull design
- preliminary design
- sizing
- lofting
- unmanned LTA
- unmanned vehicles
- low atmosphere
- deployment
- stratospheric missions
- attitude control
- motion prediction
- simulation
- optimal sizing
- automated sizing
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