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Automated design of CubeSats and small spacecrafts
Himangshu Kalita
,
Jekanthan Thangavelautham
Research output
:
Contribution to journal
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Conference article
›
peer-review
1
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Keyphrases
Design Teams
100%
Spacecraft Design
100%
Small Spacecraft
100%
Automated Design
100%
CubeSat
100%
Near-optimal Solution
66%
Mass Volume
66%
Engineering Judgment
66%
Low-mass
33%
Propellant
33%
Actuator
33%
Low Power
33%
Design Space
33%
Propulsion
33%
Design Approach
33%
Reduced Volume
33%
Reduced Mass
33%
Miniaturization
33%
Science Instruments
33%
Darwinian
33%
Earth Observation
33%
Lunar Orbit
33%
Expert Team
33%
Innovative Design
33%
Human Design
33%
Volume Power
33%
Implementation Feasibility
33%
Engineering Experience
33%
Electronic Sensors
33%
Individual Judgment
33%
Virtual Warehouse
33%
Spacecraft Engineering
33%
Fit Design
33%
Engineering Design Teams
33%
Space Robotics
33%
Optimized Design
33%
Interplanetary Mission
33%
Optimized Solution
33%
Astrophysics Applications
33%
Earth and Planetary Sciences
Spacecraft
100%
CubeSat
100%
Spacecraft Design
60%
Decision Making
40%
Actuator
20%
Limiting Factor
20%
Design Method
20%
Lunar Orbit
20%
Low Earth Orbit
20%
Robotics
20%
Astrophysics
20%
Engineering
CubeSat
100%
Spacecraft
100%
Candidate Design
50%
Engineering
25%
Limitations
12%
Design Method
12%
Design Space
12%
Systematic Approach
12%
Design Point
12%
Limiting Factor
12%
Warehouses
12%
Engineering Judgement
12%
Earth Observation Mission
12%
Space Robotics
12%
Actuator
12%
Low Earth Orbit
12%
Physics
Spacecraft
100%
CubeSat
100%
Spacecraft Design
60%
Lunar Orbit
20%
Actuator
20%
Astrophysics
20%
Science Instrument
20%