Investigation of an Electrospray within a Cold Gas Nozzle for a Dual-Mode Thruster

Little, Bryan; Jugroot, Manish

doi:10.2514/6.2017-5038

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Propulsive Device1

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2020

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“…But cold gas propulsion systems are the lowest in cost with the simplest mechanical structure and in turn, the most developed. [72][73][74][75] The existing literature summarized the micropropulsion technologies 7,76,77 and electric propulsion systems. 8,70 Tummala and Dutta in their study 7 reviewed the Cubesat-related technologies (i.e.…”

Section: Propulsive Devicementioning

confidence: 99%

Developments of attitude determination and control system of microsats: A survey

Ma²,

Guo

et al. 2020

Proceedings of the Institution of Mechanical Engineers, Part I:

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This study surveys the developments in satellite attitude determination and control system, especially for microsats. This survey is not intended to be complete but is limited to the most significant developments of sensors, actuators, and algorithms in the last two decades. First, attitude determination methods including algorithms and sensors together with actuator-based control methods are introduced. Furthermore, current problems in alignment error, flexible satellites, and low redundancy of microsats attitude determination and control system are discussed. Moreover, developments of some deep-neural-networks-based methods, which have great potential in solving current problems, are summarized.

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