Spacecraft development testbed system

• US 8,977,391 B2
• Filed: 07/15/2011
• Issued: 03/10/2015
• Est. Priority Date: 07/15/2011
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Vavrina, Matthew Aaron, Vian, John Lyle
• Primary Examiner(s): Tran, Khoi
• Assistant Examiner(s): Figueroa, Jaime
• Application Number:
  US13/183,618
• Publication Number:
  US 20130017838A1
• Time in Patent Office: 1,334 Days
• Field of Search: 700/245, 702/1, 702/108, 702/113, 702/127, 702/144, 702/187, 702/189, 701/1, 701/36, 703/7, 703/8, 244/158.1
• US Class Current: 700/245
• CPC Class Codes: B64G 7/00 Simulating cosmonautic conditions, e.g. for conditioning crews

Abstract

A method and apparatus comprising a location reference system and a control module. The location reference system is configured to generate location information for a number of mobile platforms in an environment. The control module is configured to receive the location information for the number of mobile platforms from the location reference system. The control module is further configured to generate command signals for the number of mobile platforms using the location information. The control module is further configured to send the command signals to the number of mobile platforms to operate the number of mobile platforms in the environment such that operation of the number of mobile platforms emulates the operation of a number of spacecraft systems in a non-Earth terrestrial environment.

Claims

1. An apparatus comprising:

a location reference system configured to generate location information comprising position and orientation information for a number of mobile platforms in an environment, the position information including a three dimensional position of a mobile platform with respect to a reference point, and the orientation information including an angular rotation of a mobile platform with respect to a number of axes;

a processor configured to identify characteristics for movement of a number of spacecraft in a non-Earth environment and to consider a number of conditions for the non-Earth environment in identifying the characteristics for movement; and

a control module configured to identify characteristics for movement of the number of mobile platforms in the non-Earth terrestrial environment, to receive the location and orientation information for the number of mobile platforms from the location reference system;

to generate command signals for the number of mobile platforms using the location and orientation information and the characteristics identified for the movement of the number of mobile platforms and the characteristics for movement of the number of spacecraft; and

to send the command signals to the number of mobile platforms to operate the number of mobile platforms in the environment such that operation of the number of mobile platforms emulates operation of the number of spacecraft systems in the non-Earth terrestrial environment, the command signals including commands to operate the number of mobile platforms on a surface representing terrain of the non-Earth terrestrial environment, at least a portion of the control module positioned remotely from the number of mobile platforms.

2. The apparatus of claim 1 further comprising:

the number of mobile platforms, wherein the number of mobile platforms is configured to operate within the environment to emulate the operation of the number of spacecraft systems when the number of spacecraft systems is operating in the non-Earth terrestrial environment, wherein the command signals include commands to operate the number of mobile platforms on an uneven surface representing terrain of the non-Earth environment and commands for the number of mobile platforms to fly over the surface, and wherein the location reference system;

the control module configured and to generate simulated data for a first number of systems for the number of spacecraft.

3. The apparatus of claim 2, wherein the number of spacecraft systems includes a first number of systems and further comprising:

a second number of systems associated with the number of mobile platforms, wherein the command signals are sent to the second number of systems to cause the second number of systems to emulate operation of the first number of systems in the non-Earth terrestrial environment, the simulated data for the first number of systems for the number of spacecraft generated without using the second number of systems associated with the number of mobile platforms.

4. The apparatus of claim 1 further comprising:

a data management module configured to record the location information for the number of mobile platforms in the environment.

5. The apparatus of claim 4, wherein the data management module is configured to store data generated by a second number of systems associated with the number of mobile platforms.

6. The apparatus of claim 1 further comprising:

a health monitoring module configured to receive health monitoring information from the number of mobile platforms and monitor a health condition for the number of mobile platforms based on the health monitoring information received, wherein the command signals are generated by the control module based on the health condition for the number of mobile platforms.

7. The apparatus of claim 1, wherein the command signals are first command signals and wherein the control module is configured to send second command signals to the number of spacecraft systems in the non-Earth terrestrial environment to control the operation of the number of spacecraft systems in the non-Earth terrestrial environment.

8. The apparatus of claim 1, wherein a system in the number of spacecraft systems comprises at least one of software and hardware and wherein the system in the number of spacecraft systems is selected from one of a sensor system, a position identification system, a camera system, a propulsion system, a thruster system, a docking system, a landing system, a movement system, a power system, a communication system, and a control system.

9. The apparatus of claim 3, wherein the first number of systems comprises at least one of software and hardware and wherein a system in the first number of systems and the second number of systems is selected from one of a sensor system, a position identification system, a camera system, a propulsion system, a thruster system, a docking system, a landing system, a movement system, a control system, a power system, and a communications system.

10. The apparatus of claim 1, wherein a spacecraft system in the number of spacecraft systems is selected from one of a space vehicle, a satellite, a space shuttle, a planetary landing vehicle, an orbiting spacecraft, an Earth-orbiting spacecraft, a manned spacecraft, an unmanned spacecraft, a space station, a rocket, a space missile, a space probe, a space robot, a space suit, a space platform, a space device, and a space assembly.

11. A system for developing and testing a number of spacecraft systems comprising:

a number of mobile platforms configured to operate within an environment to emulate operation of the number of spacecraft systems in a non-Earth terrestrial environment;

a location reference system configured to generate location information and orientation information for the number of mobile platforms in the environment, the location information including a three dimensional position of a mobile platform with respect to a reference point, and the orientation information including an angular rotation of a mobile platform with respect to a number of axes;

a health monitoring module configured to receive health monitoring information from the number of mobile platforms and to monitor a health condition for the number of mobile platforms using the health monitoring information received;

a processor configured to identify characteristics for movement of a number of spacecraft in a non-Earth environment and to consider a number of conditions for the non-Earth environment in identifying the characteristics for movement;

a control module configured to identify characteristics for movement of the number of mobile platforms in the non-Earth terrestrial environment, to receive the location information and the orientation information for the number of mobile platforms from the location reference system;

to generate command signals for the number of mobile platforms using the location information, the orientation information, the characteristics for movement of the number of mobile platforms in the non-Earth terrestrial environment, the characteristics for movement of the number of spacecraft, and the health condition for the number of mobile platforms;

to send the command signals to the number of mobile platforms to operate the number of mobile platforms in the environment such that operation of the number of mobile platforms emulates the operation of the number of spacecraft systems in the non-Earth terrestrial environment; and

to generate simulated data for a first number of systems for the number of spacecraft, the command signals including commands to operate the number of mobile platforms on a surface representing terrain of the non-Earth terrestrial environment, at least a portion of the control module positioned remotely from the number of mobile platforms; and

a data management module configured to record the location information for the number of mobile platforms in the environment.

12. The system of claim 11, wherein the number of spacecraft systems includes the first number of systems and further comprising:

a second number of systems associated with the number of mobile platforms, wherein the command signals are sent to the second number of systems to cause the second number of systems to emulate operation of the first number of systems when the first number of systems is operating in the non-Earth terrestrial environment, the simulated data for the first number of systems for the number of spacecraft generated without using the second number of systems associated with the number of mobile platforms.

13. The system of claim 11, wherein a spacecraft system in the number of spacecraft systems is selected from one of a space vehicle, a satellite, a space shuttle, a planetary landing vehicle, an orbiting spacecraft, an Earth-orbiting spacecraft, a manned spacecraft, an unmanned spacecraft, a space station, a rocket, a space missile, a space probe, a space robot, a space suit, a space platform, a space device, and a space assembly.

14. A method for testing a number of spacecraft systems, the method comprising:

a computer identifying characteristics for movement of a number of mobile platforms in a non-Earth terrestrial environment;

the computer configured to identify characteristics for movement of a number of spacecraft in the non-Earth terrestrial environment and to consider a number of conditions for the non-Earth terrestrial environment in identifying the characteristics for movement of the number of spacecraft;

the computer receiving location information and orientation information for the number of mobile platforms in an environment, wherein the location information and the orientation information are generated using a location reference system, the location information including a three dimensional position of a mobile platform with respect to a reference point, and the orientation information including an angular rotation of a mobile platform with respect to a number of axes;

the computer generating command signals for the number of mobile platforms using the location information, the orientation information, the characteristics for movement of the number of mobile platforms in the non-Earth terrestrial environment, and the characteristics for movement of the number of spacecraft;

the computer generating simulated data for a first number of systems for the number of spacecraft; and

the computer sending the command signals to the number of mobile platforms to operate the number of mobile platforms in the environment such that operation of the number of mobile platforms emulates operation of the number of spacecraft systems in the non-Earth terrestrial environment, the command signals including commands to operate the number of mobile platforms on a surface representing terrain of the non-Earth terrestrial environment, at least a portion of the control module positioned remotely from the number of mobile platforms.

15. The method of claim 14, wherein the number of spacecraft systems comprises a first number of systems and wherein sending the command signals to the number of mobile platforms comprises:

the computer sending the command signals to a second number of systems associated with the number of mobile platforms to cause the second number of systems to emulate operation of the first number of systems in the non-Earth terrestrial environment, the simulated data for the first number of systems for the number of spacecraft generated without using the second number of systems associated with the number of mobile platforms.

16. The method of claim 14 further comprising:

the computer recording the location information for the number of mobile platforms in the environment.

17. The method of claim 15 further comprising:

the computer storing data generated by the second number of systems during operation of the second number of systems while the number of mobile platforms is moving in the environment.

18. The method of claim 14 further comprising:

the computer receiving health monitoring information from the number of mobile platforms;

the computer monitoring a health condition for the number of mobile platforms based on the health monitoring information received; and

wherein the step of generating the command signals comprises;

the computer generating the command signals using the location information and the health condition for the number of mobile platforms.

19. The method of claim 14, wherein the command signals are first command signals and further comprising:

the computer sending second command signals to the number of spacecraft systems in the non-Earth terrestrial environment to control the operation of the number of spacecraft systems in the non-Earth terrestrial environment.

20. The method of claim 14, wherein a spacecraft in the number of spacecraft systems is selected from one of a space vehicle, a satellite, a space shuttle, a planetary landing vehicle, an orbiting spacecraft, an Earth orbiting spacecraft, a manned spacecraft, an unmanned spacecraft, a space station, a rocket, a space missile, a space probe, a space robot, a space suit, a space platform, a space device, and a space assembly.