초록 ▼

An integrated power and attitude control system that includes a plurality of flywheels and a controller. The controller receives power commands and attitude commands and determines the optimum set of flywheel acceleration and gimbal velocity commands to supply to each flywheel, to meet the commanded

An integrated power and attitude control system that includes a plurality of flywheels and a controller. The controller receives power commands and attitude commands and determines the optimum set of flywheel acceleration and gimbal velocity commands to supply to each flywheel, to meet the commanded power and attitude. Flywheel rotational acceleration is controlled to provide the commanded power, and both flywheel acceleration and flywheel gimbal angular velocity are controlled to provide the commanded attitude.

대표청구항 ▼

1. An integrated power and attitude control system, comprising:a controller coupled to receive at least a torque command signal and a power command signal and operable, in response thereto, to supply (i) a gimbal angular velocity command based at least in part on the torque command signal and (ii) a

1. An integrated power and attitude control system, comprising:a controller coupled to receive at least a torque command signal and a power command signal and operable, in response thereto, to supply (i) a gimbal angular velocity command based at least in part on the torque command signal and (ii) a flywheel acceleration command based at least in part on the torque command signal and the power command signal; anda flywheel system coupled to receive the gimbal angular velocity command and the flywheel acceleration command from the controller and operable, in response thereto, to (i) move at the commanded gimbal angular velocity on a gimbal axis and (ii) accelerate at the commanded flywheel acceleration on a spin axis. 2. The system of claim 1, wherein the flywheel system is further operable to supply a gimbal angular velocity feedback signal, and wherein the controller comprises:a torque prediction circuit coupled to receive the gimbal angular velocity feedback signals from each energy storage flywheel system and operable, in response thereto, to supply a predicted torque output signal;a comparator circuit coupled to receive the torque command signal and the predicted torque output signal and operable, in response thereto, to supply a torque control input signal; anda speed control circuit coupled to receive the torque control input signal and the power command signal and operable, in response thereto, to supply the flywheel acceleration command. 3. The system of claim 1, wherein the controller comprises:a gimbal control circuit coupled to receive the torque command signal and operable, in response thereto, to supply the gimbal angular velocity command. 4. The system of claim 1, wherein the flywheel system further includes:one or more magnetic bearings rotationally mounting the flywheel system; anda magnetic bearing controller coupled to receive bearing command signals and operable, in response thereto, to supply position control signals to each of the magnetic bearings. 5. The system of claim 1, wherein each flywheel system further includes:a motor/generator coupled to the flywheel system to supply rotational energy to, and receive rotational energy from, the flywheel system; anda motor/generator controller coupled to receive the flywheel acceleration command and operable, in response thereto, to supply operational control signals to the motor/generator to thereby accelerate the flywheel system. 6. The system of claim 1, wherein each flywheel system is mounted in a gimbal frame, and wherein the system further comprises:one or more actuators coupled to receive the gimbal angular velocity command signal from the controller and operable, in response thereto, to move the gimbal frame to the gimbal angle at the commanded angular velocity. 7. The system of claim 1, wherein the controller and flywheel system are each mounted within a vehicle, and wherein the system further comprises:an attitude sensor mounted within the vehicle and adapted to sense an attitude of the vehicle relative to a reference, the attitude sensor supplying a position feedback signal to the controller,wherein the controller is responsive to the position feedback signal to thereby adjust at least the gimbal angular velocity command signal to achieve the commanded torque. 8. The system of claim 7, wherein:the vehicle has multiple degrees of freedom;the controller is operable to supply independent gimbal angular velocity commands and independent flywheel acceleration commands for at least each of the vehicle degrees of freedom; andthe system further comprises:a plurality of flywheel systems, each flywheel system coupled to receive one of the independent gimbal angular velocity commands and one of the independent flywheel acceleration commands. 9. The system of claim 8, wherein the system comprises four or more flywheel systems. 10. The method of controlling the relative attitude and rotational speed of a flywheel, comprising:receiving a torque command signal and a power command signal;supplying a gimbal angular velocity command based at least in part on the torque command;supplying a rotational acceleration command based at least in part on the torque command signal and the power command signal;moving the flywheel at the commanded gimbal angular velocity on a gimbal axis; androtationally accelerating the flywheel at the commanded rotational acceleration on a spin axis. 11. The method of claim 10, further comprising:supplying a gimbal angular velocity feedback signal from the flywheel;supplying a predicted torque output signal based at least in part on the gimbal angular velocity feedback signal;comparing the predicted torque output signal to the torque command signal and, based at least in part thereon, supplying a torque control input signal; andsupplying the rotational acceleration command based at least in part on the torque control input signal and the power command signal. 12. The method of claim 10, wherein the flywheel is mounted within a vehicle, and wherein the method further comprises:supplying a vehicle position feedback signal based on a sensed attitude of the vehicle relative to a reference; andadjusting at least the gimbal angular velocity command signal in response to the position feedback signal to thereby to achieve the commanded torque. 13. A satellite, comprising:a controller coupled to receive at least a torque command signal and a power command signal and operable, in response thereto, to supply (i) one or more independent gimbal angular velocity commands based at least in part on the torque command signal and (ii) one or more independent flywheel acceleration commands based at least in part on the torque command signal and the power command signal; anda plurality of energy storage flywheel systems, each flywheel system coupled to receive one of the gimbal angular velocity commands and one of the flywheel acceleration commands from the controller and operable, in response thereto, to (i) move on a gimbal axis at the commanded gimbal angular velocity it received and (ii) accelerate on a spin axis at the commanded flywheel acceleration it received.