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CubeSat Design and Attitude Control with Micro Pulsed Plasma Thrusters

Palavra-chave:

attitude control, Pulsed Plasma Thrusters, and CubeSat

O Criador:

Lu, Ye

Advisor:

Gatsonis, Nikolaos A.

Editor:

Worcester Polytechnic Institute

Data Criada:

2015-04-29

Resource Type:

Thesis

Degree:

MS

Unit (Department):

Mechanical Engineering