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Trajectory Options for Low-Cost Missions to Easily Retrievable Objects
By: Dong Qiao and Colin R. McInnes.
Pub. 2015,
12pgs.
PDF File.
14-538.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Research on Cooperative Motion Planning of Agile and Autonomous On-Orbit Servicing Spacecraft with Complicated Space Environment
By: Jifeng Guo, Jinjun Shan and Xiaobu Xue.
Pub. 2015,
9pgs.
PDF File.
14-539.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
High Fidelity Direct Transcription Method for Optimization of Many Revolution, Low-Thrust Trajectories
By: Chit Hong Yam and Yasuhiro Kawakatsu.
Pub. 2015,
12pgs.
PDF File.
14-540.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Configuration Optimization for Swarm Spacecraft Based in PSO-SQP Algorithm
By: Hu Min, Song Junling, Fan Li and Hou Zhendong.
Pub. 2015,
12pgs.
PDF File.
14-541.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Attitude Control Mechanization to De-Orbit Satellites Using Solar Sales
By: Ozan Tekinalp and Omer Atas.
Pub. 2015,
12pgs.
PDF File.
14-543.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
An Application of Adaptive Fault-Tolerant Control to Nano-Spacecraft
By: Yu Han, James Biggs and Naigang Cui.
Pub. 2015,
13pgs.
PDF File.
AAS 14-567.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
On Optimization of Parameters for Linear Stabilization Systems
By: Anna D. Guerman, Ana M. Seabra and Georgi V. Smirnov.
Pub. 2015,
8pgs.
PDF File.
14-545.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Attitude Control of a Spacecraft with a Double-Gimbal Variable-Speed Control Moment Gyro Via LPV Control Theory
By: Takahiro Sasaki and Takashi Shimomura.
Pub. 2015,
17pgs.
PDF File.
14-546.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Mixed Control Momentum Gyroscopes and Reactions Wheel Based Attitude Control System
By: E. Scorzafava, F. Covello, D. Cascone and A. Anania.
Pub. 2015,
10pgs.
PDF File.
14-547.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
Attitude Determination and Control in the T-LOGOQUBE FEMTO-Satellite Mission
By: Sean McNeil, Garrett Jernigan, Benjamin Malphrus, Kevin Brown, Robert Twiggs, William Roach-Barrett, Kevin Zack, Brian Silverman and Lynn Cominsky.
Pub. 2015,
5pgs.
PDF File.
14-548.
Price: $29.00
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.
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