摘要
说明了集成化储能与姿态控制系统的工作原理,提出了一种由两反转飞轮系统及气浮转台组成的单轴飞轮储能/姿态控制系统的原理实验装置,对姿态与DC总线电压控制进行了解耦,通过各子系统模型建立了系统的数学模型。通过仿真证明了利用两反转飞轮系统可以实现电能与动能之间的相互转化,并在能量转化的同时实现了气浮转台角度的控制,对于集成化能量与姿态控制系统实验样机的研制具有一定的指导意义。
The utilization of flywheels to integrated power and attitude control system （IPACS） in satellites to replace traditional chemical batteries and attitude control system have the benefits of increasing reliability, reducing overall weight and spacecraft size, cost. The experimental device of single axis attitude control and energy storage system with two counter rotating flywheels is designed, and the attitude control is decoupled from DC bus voltage. A computer simulation model of a flywheel energy storage and single axis attitude control system is described in this paper. The goal is to research on control method of energy storage and attitude control use flywheel system, resolve the couple problem between energy storage and attitude control, study the key technology and prepare for the test system. The simulation results demonstrate that it is possible to use two flywheels to simultaneously provide energy storage while regulating the platform attitude in a single axis.
出处
《系统仿真学报》
CAS
CSCD
北大核心
2006年第9期2511-2515,共5页
Journal of System Simulation
基金
国家863计划(2002AA715061)
民用航天预研项目
