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The trajectory planning of spacecraft based on optimal quintic polynomial
Yanghua Li,
Bo Mo
School of Aerospace Engineering
Beijing Institute of Technology
Research output
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Contribution to conference
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Paper
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peer-review
3
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Engineering
Trajectory Planning
100%
Dynamic Models
50%
Control Algorithm
50%
Periodic Time
50%
Angular Velocity ω
50%
Spacecraft Trajectory
50%
Kinematic Model
50%
Attitude Angle
50%
Angular Acceleration
50%