The Orion spacecraft as a key element in a deep space gateway

Timmons, K.K.; Coderre, Kathleen; Pratt, William D.; Cichan, Timothy

doi:10.1109/aero.2018.8396769

Cited by 7 publications

(4 citation statements)

References 1 publication

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“…The crew seats will be attached the flow structure inside Orion, which is also the stowage locker that stores the equipments. This structure is an aluminum structure of crisscrossing beams [13].…”

Section: Structurementioning

confidence: 99%

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Development and the State-of-Art Facility for Aerospace Vehicle

Gao¹

2023

HSET

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Aerospace vehicles is the platform of next generation transportation as well as a compulsory tool to investigate expletory. However, the space technology hasn’t really had a breakthrough progress. On this basis, this paper will discuss the current development history, progress as well as demonstrate the state-of-art facilities for aerospace vehicle. To be specific, the structure, propulsion and material of the aerospace vehicles in different era will be introduced with detail parameters. According to the analysis, although the core propulsion form remains unchanged as chemical propulsion, progress in safety has been almost accomplished. In addition, the thermal protection material took the advantage from old but mature technologies. To better illustrate the statements, schematically visualizations have been demonstrated. At the same time, the drawbacks and defects of current facility as well as future prospects for the improvements of the designs are proposed accordingly. Overall, these results shed light on guiding further exploration of aerospace vehicle.

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Section: Structurementioning

confidence: 99%

“…The service module uses 4 solar array wings to generate electricity that can powering 2 threebedroom homes. The service module also contains tanks storing water, oxygen and nitrogen [13].…”

Section: Structurementioning

confidence: 99%

Development and the State-of-Art Facility for Aerospace Vehicle

Gao¹

2023

HSET

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“…The FCMs have sufficient processing power to perform command and control of Orion as well as the LOP-G. Utilizing Orion as the command deck when docked with the Gateway enables a more streamlined approach to the avionics on the LOP-G. The LOP-G command and data handling can be more akin to a deep space planetary mission because it relies on the reliability and availability built into Orion [13].…”

Section: The Orion Crew Vehiclementioning

confidence: 99%

Science on the lunar surface facilitated by low latency telerobotics from a Lunar Orbital Platform - Gateway

et al. 2019

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“…During the past decades, spacecraft attitude control has become a major research topic in the aerospace domain, because it can be used to perform various advanced tasks in the aerospace domain including deep space exploration [1], space on-orbit services [2,3], and spacecraft proximity operations [4,5]. The main research issues associated with the spacecraft attitude control system design include highly nonlinear characteristics owing to the presence of rigid-flexible coupled structures [6], parameter uncertainties [7], external disturbances and actuator faults [8][9][10][11], input nonlinearity [12,13], and formation control [14][15][16].…”

Section: Introductionmentioning

confidence: 99%

Adaptive fuzzy backstepping control for attitude stabilization of flexible spacecraft with signal quantization and actuator faults

Liu

Duan

2021

Sci. China Inf. Sci.

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In this study, the fault-tolerant attitude control of flexible spacecraft is investigated over digital communication channels, where a uniform quantizer is considered with respect to the sensor signals and controller indexes. Further, an adaptive fuzzy backstepping control strategy has been developed for the considered attitude stabilization issue, where the adaptive fuzzy logic method is used to approximate the rigid-flexible coupled nonlinearity of the spacecraft. In this design, the online adjusting quantizer parameters are injected into the controller gains to simultaneously compensate for the quantization errors and timevarying actuator faults. In the proposed control method, the attitude stabilization task is achieved in the presence of external disturbances, time-varying actuator faults, and signal quantization. Finally, the practical examples are compared to demonstrate the effectiveness of the proposed control strategy.

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The Orion spacecraft as a key element in a deep space gateway

Cited by 7 publications

References 1 publication

Development and the State-of-Art Facility for Aerospace Vehicle

Development and the State-of-Art Facility for Aerospace Vehicle

Science on the lunar surface facilitated by low latency telerobotics from a Lunar Orbital Platform - Gateway

Adaptive fuzzy backstepping control for attitude stabilization of flexible spacecraft with signal quantization and actuator faults

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