Apparatus and Method for Diagnosing Fault and Managing Data in Satellite Ground System

• US 20080313488A1
• Filed: 05/24/2006
• Published: 12/18/2008
• Est. Priority Date: 09/29/2005
• Status: Active Grant

• Current Assignee: Electronics and Telecommunications Research Institute
• Original Assignee: Electronics and Telecommunications Research Institute
• Inventors: Kim, Jae-Hoon, Lee, Sang-Uk, Jeong, Seong-Kyun, Jung, Ok-Chul
• Granted Patent: US 8,131,287 B2
• Time in Patent Office: Days
• US Class Current: 714/2
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance

Abstract

Provided are an apparatus and a method for diagnosing fault and processing data of a satellite ground system. The apparatus and a method can prevent data loss of a satellite, and efficiently operate the satellite ground system using data buffer and penalty method when a temporary fault occurs. Data buffer stores data in fault situation and penalty method imposes high penalty in critical fault and low penalty in minor fault. System is managed according to penalty degree. The apparatus, includes: a satellite data processing and controlling means; a signal transforming means; a fault detecting and controlling means; a state displaying means for displaying a state of the satellite and the system; a penalty managing means for being notified whether the device has fault or not; a data storing means for storing and transmitting the data; and a system recovery supporting means.

Claims

1. An apparatus for diagnosing fault and processing data of a satellite ground system, comprising:

a satellite data processing and controlling means for processing and analyzing data transmitted from a satellite and performing control required for the satellite;

a signal transforming means for transforming a signal transmitted from the satellite and transmitting the transformed signal to the satellite ground system;

a fault detecting and controlling means for detecting fault by comparing a signal from the satellite data processing and controlling means, all data from the signal transforming means, and a state of each device with each other, and transmitting fault detect contents;

a state displaying means for displaying a state of the satellite and the system by displaying a state of the satellite data processing and controlling means, and the fault detecting and controlling means;

a penalty managing means which is notified whether the device has fault or not from the fault detecting and controlling means and processing the data based on a penalty value;

a data storing means for storing the data when an error is found by the fault detecting and controlling means, and transmitting the data based on a fault state; and

a system recovery supporting means for performing a recovery process when fault is declared in the fault detecting and controlling means.

2. The apparatus as recited in claim 1, wherein the satellite data processing and controlling means includes:

a telemetry data storing unit for storing data on which telemetry is performed by the satellite;

a telemetry data processing unit for processing telemetry data stored in the telemetry data storing unit;

a telecommand generating unit for generating a telecommand to process the satellite data; and

a telecommand verifying unit for verifying the telecommand generated in the telecommand generating unit.

3. The apparatus as recited in claim 1, wherein the fault detecting and controlling unit, includes:

a primary device data receiving unit for receiving primary device data of the satellite ground system;

a secondary device data receiving unit for receiving secondary device data of the satellite ground system; and

a comparison unit for comparing the data of the primary device data receiving unit with the data of the secondary device data receiving unit.

4. The apparatus as recited in claim 1, wherein the fault detecting and controlling means receives data individually in the primary device data receiving unit and the secondary device data receiving unit, and transmits the data individually in the dualized satellite ground system.

5. The apparatus as recited in claim 4, wherein when the data transmitted from the primary and secondary device data receiving unit are compared by the comparison unit, the fault detecting and controlling unit notifies to penalty managing unit whether the devices have an error, transmits each data to a device requiring the data when the devices have no error based on a penalty value, stores the data in the storing unit when the devices have an error and transmits the data based on a fault state.

6. The apparatus as recited in claim 4, wherein the penalty managing means transmits data of a robust buffer when a penalty value becomes larger than a fault declaration value, transmits combined buffer data when fault is temporary, immediately switches off the device when the fault is declared, has only the secondary device be used and gives a recovery command to the system recovery supporting means.

7. The apparatus as recited in claim 4, wherein the system recovery supporting means notifies a faulty device and a fault state to an operator, goes through a recovery process including testing and re-driving of the faulty device, and prevents the faulty device from being abandoned permanently by returning the device to the system when it is declared that recovery process is completed.

8. A method for diagnosing fault and processing data of a satellite ground system, comprising the steps of:

a) storing data transmitted from primary and secondary devices of the satellite ground system;

b) calculating penalty values in the penalty managing means;

c) comparing the penalty values calculated in the step b) with a predetermined fault declaration value T;

d) declaring the fault of the device when a penalty value is larger than the fault declaration value T in the step c), transmitting data of a robust device after switching the faulty device and driving the system recovery supporter; and

e) checking whether the fault of the device is temporary when the penalty value is not larger than the fault declaration value T in the step c).

9. The method as recited in claim 8, wherein in the step a), data loss is prevented by storing the transmitted data in a data buffer, and the fault declaration by the temporary fault or an error in data transmission is also prevented by transmitting the data of the robust device when the device has the fault, and combining and transmitting the data stored in the buffer when the fault is temporary.

10. The method as recited in claim 8, wherein the step b), includes the steps of:

b1) determining whether the device has fault by checking data transmitted from the primary and secondary devices if there is a difference;

b2) increasing a penalty value based on a result of the step b1) and an effect of the fault on the satellite ground system; and

b3) decreasing a present penalty value when there is no difference between data in the step b1) and no fault occurs for a predetermined time.

11. The method as recited in claim 8, wherein in the step b), a penalty record for the fault state is preserved although the fault is temporary, and the penalty record is deleted when no error occurs for a predetermined time.

12. The method as recited in claim 8, wherein in the step b), the fault is separated from the satellite ground system by imposing a fault declaration value when the fault halts or hinders operation of hardware.

13. The method as recited in claim 8, wherein in the step b), the penalty value is increased instead of separating faulty device by imposing the lowest penalty value when the fault is only a minor error.

14. The method as recited in claim 11, wherein a penalty value is imposed based on a degree of the fault in the step b) and when no fault occurs in the satellite ground system, a record on penalty is deleted and time taken for deleting the penalty record is based on the penalty value.

15. The method as recited in claim 11, wherein in the step e), the penalty value is compared with “

0”

to figure out whether the fault is temporary.

16. The method as recited in claim 11, wherein in the step e), the combined data are transmitted when the fault is temporary.

17. The method as recited in claim 11, wherein in the step e), a value of the data buffer is maintained when the fault is not temporary.

18. The method as recited in claim 11, wherein in the step e), the data of the buffer are transmitted when the penalty value is “

0”

.