Satellite Attitude Control Using Control Moment Gyroscopes
| Autor: | Róger Mateus Sehnem, Wilcker Neuwald Schinestzki, Leonardo Barros da Luz, Kenedy Matiasso Portella, Pedro Paglione, Lorenzzo Quevedo Mantovani, Tarso Kraemer Sarzi Sartori, Renan Rathis Sacco |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2020 |
| Předmět: |
0209 industrial biotechnology
Angular momentum Computer science lcsh:Motor vehicles. Aeronautics. Astronautics Aerospace Engineering 02 engineering and technology Gimbal Nonlinear control lcsh:Technology law.invention Attitude control 020901 industrial engineering & automation 0203 mechanical engineering law Control theory Torque 020301 aerospace & aeronautics lcsh:T attitude control Gyroscope linear quadratic tracker Moment (mathematics) control moment gyroscopes Control system nonlinear control lcsh:TL1-4050 exponential mapping control |
| Zdroj: | Journal of Aerospace Technology and Management, Vol 12, Iss se, Pp 94-105 (2020) |
| ISSN: | 2175-9146 1984-9648 |
| Popis: | In space missions, there is often a need for an attitude control system capable of maintaining the desired attitude. In situations that require agile and accurate responses, which also require large torques, control moment gyroscopes (CMGs) may be used. Control moment gyroscopes are high angular moment gyros mounted on gimbals and are responsible for changing the direction of the angular momentum vector, consequently generating the control torques. There are several linear and nonlinear techniques that can be employed in the design of control laws with the final choice being a compromise between simplicity, effectiveness, efficiency and robustness. The main objective of this study is to evaluate the performance of control systems techniques with 4 CMGs in a pyramidal arrangement, either by using Linear Quadratic Tracker (LQT) with integral compensator or Exponential Mapping Control (EMC). A reference attitude will be defined to be traced in the presence of disturbance torques caused by the gravitational gradient. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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