Inicio  /  Aerospace  /  Vol: 9 Par: 8 (2022)  /  Artículo
ARTÍCULO
TITULO

Design of Novel Laser Crosslink Systems Using Nanosatellites in Formation Flying: The VISION

Geuk-Nam Kim    
Sang-Young Park    
Sehyun Seong    
Jae-Young Choi    
Sang-Kook Han    
Young-Eon Kim    
Suyong Choi    
Joohee Lee    
Sungmoon Lee    
Han-Gyeol Ryu and Seonghui Kim    

Resumen

With growth in data volume from space missions, interest in laser communications has increased, owing to their importance for high-speed data transfer in the commercial and defense fields, spaceborne remote sensing, and surveillance. Here, we propose a novel system for space-to-space laser communication, a very high-speed inter-satellite link system using an infrared optical terminal and nanosatellite (VISION), which is aimed at establishing and validating miniaturized laser crosslink systems and several space technologies using two 6U nanosatellites in formation flying. An optical link budget analysis is conducted to derive the signal-to-noise ratio requirements and allocate the system budget; the optical link margin should be greater than 10 dB to guarantee communication with practical limitations. The payload is a laser transceiver with a deployable space telescope to enhance the gain of the beam transmission and reception. Nanosatellites, including precise formation flying GNC systems, are designed and analyzed. The attitude control system ensures pointing and tracking errors within tens of arcsec, and they are equipped with a propulsion system that can change the inter-satellite distance rapidly and accurately. This novel concept of laser crosslink systems is expected to make a significant contribution to the future design and construction of high-speed space-to-space networks.

 Artículos similares

       
 
Zhenlong Wu, Tianyu Zhang, Yuan Gao and Huijun Tan    
In this paper, a novel small-scale gust generator research facility was designed and examined for generating Sears-type gusts. The design scheme, integration with the wind tunnel, experiment and validation of its capability are presented in detail. To he... ver más
Revista: Aerospace

 
Roberto Scigliano, Valeria De Simone, Roberta Fusaro, Davide Ferretto and Nicole Viola    
The design of integrated and highly efficient solutions for thermal management is a key capability for different aerospace products, ranging from civil aircraft using hydrogen on board to miniaturized satellites. In particular, this paper discloses a nov... ver más
Revista: Aerospace

 
Ben Campbell and Lawrence Dale Thomas    
This article describes a new alternative approach to satellite constellation deployment by incorporating momentum exchange tethers (METs). Traditional methods of deploying satellite constellations have limitations, typically involving costly propulsion s... ver más
Revista: Aerospace

 
Daniele Granata, Alberto Savino and Alex Zanotti    
The present study aimed to investigate the capability of mid-fidelity aerodynamic solvers in performing a preliminary evaluation of the static and dynamic stability derivatives of aircraft configurations in their design phase. In this work, the mid-fidel... ver más
Revista: Aerospace

 
Yacong Wu, Jun Huang, Boqian Ji and Lei Song    
Most existing studies on aerodynamic shape optimization have not considered longitudinal trim under control surface deflection, typically achieving self-trim through a constraint of zero pitching moment or adjusting the optimized configuration for longit... ver más
Revista: Aerospace