Spacecraft Control with Redundant Effectors

1999 ◽  
Vol 31 (10) ◽  
pp. 99-110
Author(s):  
Evgeniy M. Potapenko ◽  
V. G. Bichay
Keyword(s):  
Spacecraft Control

Digitally redesigned pulse-width modulation spacecraft control

1995 ◽  
Author(s):  
Douglas Zimpfer ◽  
Leang Shieh ◽  
John Sunkel
Keyword(s):  
Pulse Width ◽  
Pulse Width Modulation ◽  
Spacecraft Control

CONCEPTUAL FOUNDATIONS OF ORGANIZATIONAL TRANSFORMATIONS OF SPACECRAFT CONTROL

2020 ◽  
Author(s):  
L. A. Fedorova ◽  
◽  
M. A. Frolov ◽  
N. V. Andreev ◽  
V. V. Anokhin ◽  
...  
Keyword(s):  
Spacecraft Control ◽  
Conceptual Foundations

scholarly journals Formal Verification of Spacecraft Control Programs

2020 ◽  
Vol 19 (5) ◽  
pp. 1-18
Author(s):  
Georgy Lukyanov ◽  
Andrey Mokhov ◽  
Jakob Lechner
Keyword(s):  
Formal Verification ◽  
Spacecraft Control ◽  
Control Programs

scholarly journals Apollo Spacecraft Control Systems

1965 ◽  
Vol 2 (1) ◽  
pp. 422-433
Author(s):  
Robert G. Chilton
Keyword(s):  
Control Systems ◽  
Spacecraft Control

Precision control moment gyroscope spacecraft control with disturbance

1997 ◽  
Author(s):  
Christopher J. Heiberg ◽  
David Bailey ◽  
Bong Wie
Keyword(s):  
Precision Control ◽  
Spacecraft Control ◽  
Control Moment Gyroscope ◽  
Control Moment

scholarly journals Design And Development Of Power And Attitude Control Subsystems For RYESAT

2021 ◽  
Author(s):  
Michael William Richard. Alger
Keyword(s):  
Attitude Control ◽  
Sliding Mode ◽  
Attitude Motion ◽  
Critical Systems ◽  
Magnetic Torque ◽  
Design And Development ◽  
Control Laws ◽  
Spacecraft Control ◽  
Standard Interface ◽  
Data Bus

This thesis describes the design and development of Ryerson University's first CubeSat (RyeSat) with a focus on power and attitude control subsystems. This satellite is intended to become the initial of a series of CubeSats built by Ryerson University to perform research in spacecraft control algorithms and actuators. RyeSat is built around a standard interface, which specifies both a data-bus and a switchable power supply system for non critical systems. To facilitate the development of this satellite a prototype power subsystem was created, programmed and tested. In addition to developing the system's architecture and power subsystem; analysis was preformed to size both reaction wheels and magnetic torquers. This analysis showed that a commercially available motor could be adapted to fulfill the attitude control requirements of a CubeSat and also showed that miniature magnetic torque rods would be more efficient that magnetic torque coils typically used on CubeSats. Finally, control laws for these actuators were designed and an adaptive nonlinear sliding mode controller for reaction wheels was applied to control the 3-axis attitude motion of RyeSat.

Sign in / Sign up

Export Citation Format

Share Document