Slew Maneuver Constraints for Agile Flexible Spacecraft Article Swipe
Michael A. Marshall
,
Sergio Pellegrino
·
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.2514/1.g007430
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.2514/1.g007430
Traditional spacecraft design paradigms rely on stiff bus structures with comparatively flexible appendages. More recent trends, however, trade deployed stiffness for packaging efficiency to stow apertures with larger areas inside existing launch vehicles. By leveraging recent advances in materials and structures, these spacecraft may be up to several orders of magnitude lighter and more flexible than the current state of the art. Motivated by the goal of achieving agility despite structural flexibility, this paper proposes and verifies a quantitative method for determining structure-based performance limits for maneuvering flexible spacecraft. The results demonstrate that, contrary to common assumptions, other constraints impose more restrictive limits on maneuverability than the dynamics of the structure. In particular, it is shown that an attitude control system’s available angular momentum and torque are often significantly more limiting than the compliance of the structure. Consequently, these results suggest that there is an opportunity to design less-conservative, higher-performance space systems that can either be maneuvered faster (assuming suitable actuators are available) or built using lighter-weight, less-stiff architectures that move the structure-based performance limits closer to those of the rest of the system.
Related Topics
Concepts
Spacecraft
Agile software development
Flexibility (engineering)
Actuator
Torque
Computer science
Stiffness
Aerospace engineering
Control theory (sociology)
Engineering
Control (management)
Structural engineering
Physics
Mathematics
Artificial intelligence
Thermodynamics
Statistics
Software engineering
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.2514/1.g007430
- https://arc.aiaa.org/doi/pdf/10.2514/1.G007430?download=true
- OA Status
- bronze
- Cited By
- 4
- References
- 55
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4387097156
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W4387097156Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.2514/1.g007430Digital Object Identifier
- Title
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Slew Maneuver Constraints for Agile Flexible SpacecraftWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2023Year of publication
- Publication date
-
2023-09-27Full publication date if available
- Authors
-
Michael A. Marshall, Sergio PellegrinoList of authors in order
- Landing page
-
https://doi.org/10.2514/1.g007430Publisher landing page
- PDF URL
-
https://arc.aiaa.org/doi/pdf/10.2514/1.G007430?download=trueDirect link to full text PDF
- Open access
-
YesWhether a free full text is available
- OA status
-
bronzeOpen access status per OpenAlex
- OA URL
-
https://arc.aiaa.org/doi/pdf/10.2514/1.G007430?download=trueDirect OA link when available
- Concepts
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Spacecraft, Agile software development, Flexibility (engineering), Actuator, Torque, Computer science, Stiffness, Aerospace engineering, Control theory (sociology), Engineering, Control (management), Structural engineering, Physics, Mathematics, Artificial intelligence, Thermodynamics, Statistics, Software engineeringTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
4Total citation count in OpenAlex
- Citations by year (recent)
-
2025: 3, 2024: 1Per-year citation counts (last 5 years)
- References (count)
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55Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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