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Attitude control and stabilization of spacecraft with a captured asteroid
Saptarshi Bandyopadhyay
, Soon Jo Chung
, Fred Y. Hadaegh
Aerospace Engineering
Coordinated Science Lab
Research output
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Chapter in Book/Report/Conference proceeding
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Conference contribution
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Keyphrases
Actuator Saturation
12%
Aeronautics
12%
Asteroid Redirect Mission
75%
Asteroids
100%
Attitude Control
100%
Attitude Stabilization
100%
Control Challenges
12%
Control Law
75%
Control Strategy
25%
Control Torque
12%
Design Guidelines
12%
Disturbance Torque
12%
Earth-Moon System
12%
Exponential Convergence
12%
Fuel-optimal
12%
Fundamental Limitations
12%
Good Strategies
12%
Linear Control
37%
Measurement Error
12%
Measurement Uncertainty
12%
Mission Concept
12%
Modeling Uncertainty
50%
Near-Earth Orbit
50%
Nonlinear Tracking Control
12%
Online System Identification
12%
Optimal References
12%
Proportional-derivative
25%
Reference Trajectory
12%
Robust Nonlinear Tracking Control
25%
Space Capture
12%
Special Design
12%
Three-axis
12%
Tracking Control Law
37%
Tumbling
25%
Engineering
Actuator
11%
Attitude Control
100%
Control Law
100%
Control Strategy
22%
Design Guideline
11%
Disturbance Torque
11%
Linear Controller
33%
Measurement Error
11%
Moon System
11%
NASA
11%
Reference Trajectory
11%