Nonlinear model predictive control applied to spacecraft attitude control (Closed-loop stability and optimality with thrusters and wheels)
This paper studies model predictive control (MPC) for spacecraft nonlinear attitude control with actuator input nonlinearities. This technology is important to achieve high-rate large angle attitude maneuver problems of recent spacecraft missions. To this end, we first derive linear matrix inequalit...
| Автори: | , , , |
|---|---|
| Формат: | Стаття |
| Мова: | Japanese |
| Опубліковано: |
The Japan Society of Mechanical Engineers
2016-10-01
|
| Серія: | Nihon Kikai Gakkai ronbunshu |
| Предмети: | |
| Онлайн доступ: | https://www.jstage.jst.go.jp/article/transjsme/82/842/82_16-00198/_pdf/-char/en |