Feedback Control Law Design for the Dual-Spin Turn of Spacecraft
| Autor: | Sungkyu Kim, Hyochoong Bang, Han Hwangbo |
|---|---|
| Rok vydání: | 1997 |
| Předmět: |
Engineering
Spacecraft business.industry Applied Mathematics Rotation around a fixed axis Aerospace Engineering Angular velocity Optimal control Reaction wheel Control moment gyroscope Space and Planetary Science Control and Systems Engineering Control theory Law Physics::Space Physics Torque Electrical and Electronic Engineering business Spin (aerodynamics) |
| Zdroj: | Journal of Guidance, Control, and Dynamics. 20:450-456 |
| ISSN: | 1533-3884 0731-5090 |
| DOI: | 10.2514/2.4096 |
| Popis: | A new feedback control law design for the dual-spin turn maneuver of spinning spacecraft is discussed. The control law design study is motivated by stability analysis of dual-spin spacecraft. The feedback control law is based on the relationship between nutational stability and system energy associated with the rotational motion of spacecraft and a momentum wheel. The applied torque to the momentum wheel is adjusted in a feedback control form, for which the control law is expressed as a function of spacecraft angular velocity components, as well as the momentum wheel speed. Furthermore, a two-stage control strategy, which consists of conventional open-loop maneuver and a new feedback technique, is developed. The new strategy is verie ed by simulation study using Koreasat mass property data. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|