c-CMG Cluster for Small Satellites

Lee, Seung-Mok; Seo, Hyun-Ho; Rhee, Seung-Wu

doi:10.5139/ijass.2007.8.1.105

International Journal of Aeronautical and Space Sciences

2007

DOI: 10.5139/ijass.2007.8.1.105

|View full text |Cite

c-CMG Cluster for Small Satellites

Seung-Mok Lee¹,

Hyun-Ho Seo²,

Seung-Wu Rhee³

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2016

2024

Publication Types

Select...

Article2

Relationship

Self Cite0

Independent2

Authors

Journals

Cited by 2 publications

References 7 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Enhancing Human Comfort in eVTOL Aircraft Assisted by Control Moment Gyroscopes

Bhalla,

Kim,

Choi

2024

Int. J. Aeronaut. Space Sci.

View full text Add to dashboard Cite

This study investigates the integration of Control Moment Gyroscopes (CMGs) to enhance the comfort of human occupants in electric Vertical Take-Off and Landing (eVTOL) aircraft. Our study encompasses not only the development of a dynamic model for the eVTOL by integrating the CMGs but also the implementation of backstepping sliding mode-based controllers for translation and attitude control. To simulate realistic disturbance scenarios, wind disturbance models and a motor dynamics model are considered to replicate practical rotor responses. To validate the performance of the proposed approach, comprehensive Monte-Carlo simulations under varying wind conditions are performed. In particular, the aircraft oscillations are analyzed in the frequency domain to focus on a specific frequency that causes human discomfort. The simulation results demonstrate that the use of CMGs not only alleviates oscillations induced by wind disturbances with low power consumption but also significantly enhances passenger comfort.

show abstract

Enhancing Human Comfort in eVTOL Aircraft Assisted by Control Moment Gyroscopes

Bhalla,

Kim,

Choi

2024

Int. J. Aeronaut. Space Sci.

View full text Add to dashboard Cite

show abstract

Attitude Control System Design & Verification for CNUSAIL-1 with Solar/Drag Sail

Yoo¹,

Kim²,

Suk³

et al. 2016

International Journal of Aeronautical and Space Sciences

View full text Add to dashboard Cite

CNUSAIL-1, to be launched into low-earth orbit, is a cubesat-class satellite equipped with a 2 m × 2 m solar sail. One of CNUSAIL's missions is to deploy its solar sail system, thereby deorbiting the satellite, at the end of the satellite's life. This paper presents the design results of the attitude control system for CNUSAIL-1, which maintains the normal vector of the sail by a 3-axis active attitude stabilization approach. The normal vector can be aligned in two orientations: i) along the antinadir direction, which minimizes the aerodynamic drag during the nadir-pointing mode, or ii) along the satellite velocity vector, which maximizes the drag during the deorbiting mode. The attitude control system also includes a B-dot controller for detumbling and an eigen-axis maneuver algorithm. The actuators for the attitude control are magnetic torquers and reaction wheels. The feasibility and performance of the design are verified in high-fidelity nonlinear simulations.

show abstract

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

c-CMG Cluster for Small Satellites

Cited by 2 publications

References 7 publications

Enhancing Human Comfort in eVTOL Aircraft Assisted by Control Moment Gyroscopes

Enhancing Human Comfort in eVTOL Aircraft Assisted by Control Moment Gyroscopes

Attitude Control System Design & Verification for CNUSAIL-1 with Solar/Drag Sail

Contact Info

Product

Resources

About