Satellite simulator

• US 6,048,366 A
• Filed: 10/26/1998
• Issued: 04/11/2000
• Est. Priority Date: 10/26/1998
• Status: Expired due to Term

• Current Assignee: Peraton, Inc.
• Original Assignee: Harris-Exigent, Inc. (L3Harris Technologies, Inc.)
• Inventors: Ellis, John R., Weber, Christopher O.
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): FREJD, RUSSELL WARREN
• Application Number:
  US09/178,713
• Time in Patent Office: 533 Days
• Field of Search: 395/500.29, 395/500.43, 701/13, 375/214, 375/224, 340/825, 340/825.06, 455/3.2, 455/13.2, 455/430
• US Class Current: 703/8
• CPC Class Codes: G09B 9/00 Simulators for teaching or training purposes for the use of weapons F41; computing aspects G06; protocols for games, networked simulations or virtual reality H04L67/131
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance

Abstract

A satellite simulator to aid in the development and test of a spacecraft command and telemetry application for ground stations permits a satellite simulator to be implemented effectively and with less cost than has traditionally been possible with customized systems. From the spacecraft command and telemetry processing system, the present invention appears as a satellite that can provide a configurable telemetry stream and can accept configurable commands. The invention provides core satellite simulation capabilities required for ground station spacecraft command and telemetry processing systems such as OS/COMET or for large-scale simulation networks such as multi-service simulation systems. The present invention offers an inexpensive risk mitigation that relieves application developers of total dependency on the satellite simulation development schedule. Moreover, the present invention can be used to demonstrate the features of ground station application systems. Finally, the present invention training driver can be easier to manage and can be maintained by the training team who can rely upon the knowledge that the training exercises will function properly when presented to a training class.

Claims

1. A satellite simulator adapted for use with a plurality of satellite ground stations, said satellite simulator comprising:

a distributed messaging system for providing communications among a plurality of separate modules comprising said simulator, said distributed messaging system configured for providing communication between said modules installed on both a single host and multiple host computers;

an application specific telemetry output module configurable for data transmission to any one of a plurality of satellite ground station data acquisition systems;

an application specific command input module configurable for receiving data from any one of a plurality of satellite ground station data transmission systems; and

,

whereby said satellite simulator can simulate different satellites and satellite constellations for exercising different ones of said plurality of satellite ground stations.

2. The satellite simulator of claim 1, further comprising a bi-directional communications channel between said plurality of satellite ground stations and said satellite simulator for enabling passage of uplink command streams and downlink telemetry streams.

3. The satellite simulator according to claim 2, wherein said bi-directional communications channel is selected from one of the group consisting of an OS/COMET software bus, System V sockets, an RS-232 or RS-422 serial data link.

4. The satellite simulator of claim 1, further comprising:

a command sequencer module responsive to said application specific input module; and

,

said application specific command input module being further configurable for enabling communications between said any one of said plurality of satellite ground station data transmission systems and said command sequencer module.

5. The satellite simulator of claim 4, wherein said command sequencer module further comprises:

a plurality of predetermined user-defined commands;

a plurality of predetermined user-defined actions; and

,

means for associating said plurality of predetermined user-defined commands with said plurality of predetermined user-defined actions.

6. The satellite simulator of claim 5, wherein said associating means comprises a database containing said plurality of predetermined user-defined commands and said plurality of predetermined user-defined actions.

7. The satellite simulator of claim 1, further comprising:

a telemetry data stream formatter module, said application specific telemetry output module being responsive to said telemetry data stream formatter module; and

,

said application specific telemetry output module being further configurable for enabling communications between said telemetry data stream formatter module and said any one of said plurality of satellite ground station data acquisition systems.

8. The satellite simulator of claim 7, further comprising:

a telemetry data stream generator linked to a user interface; and

,

said telemetry data stream formatter module being responsive to said telemetry data stream generator.

9. The satellite simulator of claim 8, wherein said telemetry data stream generator further comprises:

a plurality of user-controlled and user-defined data generation sources; and

,

means for selecting a data generating function from said plurality of user-controlled and user-defined data generation sources.

10. The satellite simulator of claim 9, wherein said telemetry data stream formatter module further comprises a user-defined commutation table for describing proper multiplexing of individual measurands in a telemetry stream,

whereby said user-defined commutation table corresponds to a ground station application system decommutation table used for properly extracting said properly multiplexed individual measurands in said telemetry stream.

11. The satellite simulator of claim 8, wherein said telemetry data stream generator further comprises an external application specific telemetry data generator module for providing an external telemetry data source.

12. The satellite simulator of claim 11, further comprising an external application specific command processing module for transmitting commands to said external application specific telemetry data generator module.

13. The satellite simulator of claim 1, further comprising:

a scripting language; and

,

a processor for interpreting and executing directives of said scripting language.

14. A satellite simulator adapted for use with a plurality of satellite ground stations, said satellite simulator comprising:

a distributed messaging system for providing communications among a plurality of separate functional modules comprising said simulator, said distributed messaging system configured for providing communication between said modules installed on both a single host and multiple host computers;

a telemetry stream generator module for selectively generating a telemetry data stream;

a telemetry data stream formatter for receiving said telemetry data stream from said telemetry data stream generator and further comprising output interface means for providing said telemetry data stream to an application specific telemetry output module in a predetermined format; and

a command sequencer module comprising a plurality of predetermined user commands, a plurality of user defined action actions, and means for associating said plurality of predetermined user defined commands with said plurality of predetermined user defined actions, said command sequencer module further comprising input interface means for receiving command data in a predefined format from an application specific input module;

whereby said satellite simulator can simulate different satellites and satellite constellations for exercising different ones of said plurality of satellite ground stations.

15. A method for providing a phased implementation of a satellite simulator for use with a ground station application development program, said method comprising the steps of:

developing a ground station application comprising at least one of a telemetry processing application system and a command generation application system;

concurrently developing at least one of an application specific telemetry output module and an application specific command input module for said satellite simulator, said application specific telemetry output module and command input module each configured for communication with said ground station utilizing a computer network messaging system;

operating said satellite simulator to test said ground station application.

16. The method according to claim 15 wherein said computer network messaging system is selected from the group consisting of an OS/COMET software bus, System V sockets, an RS-232 or RS-422 serial data link.

17. The method according to claim 15 further comprising the step of modifying said application specific telemetry output module and said application specific command input module as said ground station application is developed to more closely simulate a pre-defined RF telemetry link designated for providing actual communications between said ground station application and an actual satellite to be used therewith.

18. The method according to claim 17 wherein said satellite simulator further comprises a distributed messaging system, a telemetry stream generator and a command sequencer module.

19. The method according to claim 18 further comprising the step of implementing at least one sub-module comprising said telemetry stream generator on a host computer separate from at least one of said application specific telemetry output module and said application specific command input module.

20. The method according to claim 17 further comprising the step of implementing at least one sub-module comprising said command sequencer module on a host computer separate from at least one of said application specific telemetry output module and said application specific command input module.