Virtualization-enabled satellite platforms

• US 9,876,563 B1
• Filed: 03/15/2017
• Issued: 01/23/2018
• Est. Priority Date: 10/19/2016
• Status: Active Grant

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Vector Launch, Inc.
• Inventors: Coleman, Shaun, Garber, Darren D.
• Primary Examiner(s): Lee, John J
• Application Number:
  US15/459,472
• Time in Patent Office: 314 Days
• Field of Search: 455430, 455 302, 455427, 455428, 4554521, 455 121, 455 133
• CPC Class Codes: G06F 2009/45579 I/O management, e.g. providing access to device drivers or storage
• CPC Class Codes: G06F 2009/45583 Memory management, e.g. access or allocation
• CPC Class Codes: G06F 9/45558 Hypervisor-specific management and integration aspects
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance
• CPC Class Codes: H04B 7/18521 Systems of inter linked satellites, i.e. inter satellite service for optical links between satellites H04B10/118
• CPC Class Codes: H04L 41/0668 by dynamic selection of recovery network elements, e.g. replacement by the most appropriate element after failure
• CPC Class Codes: H04L 67/10 in which an application is distributed across nodes in the network software deployment G06F8/60; multiprogramming arrangements G06F9/46
• CPC Class Codes: H04L 67/1078 Resource delivery mechanisms
• CPC Class Codes: H04L 67/125 involving control of end-device applications over a network
• CPC Class Codes: H04L 67/34 involving the movement of software or configuration parameters network booting or remote initial program loading [RIPL] G06F9/4416

Abstract

Systems, methods, and software described herein provide enhancements for deploying applications in satellite systems. In one example, a satellite system comprises a communication interface configured to receive software payloads, and a satellite control system configured to operate logistical control elements of the satellite system. The satellite system further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system.

Claims

1. A satellite system, comprising:

a communication interface configured to receive software payloads for execution by the satellite system;

a satellite control system configured to operate logistical control elements of the satellite system; and

a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system, maintain state information related to execution of ones of the virtual nodes, and transfer the state information over the communication interface for delivery to at least one peer satellite system configured as a backup to the satellite system.

2. The satellite system of claim 1, comprising:

the virtualized execution system configured to execute the ones of the software payloads as the associated virtual nodes on the satellite system according to at least a resource schedule that indicates a timewise allocation of the associated virtual nodes to the resources of the satellite system.

3. The satellite system of claim 2, comprising:

the communication interface configured to receive the resource schedule and the software payloads over at least one of a ground communication portion and an inter-satellite communication portion of the communication interface, wherein the ground communication portion communicates with a ground-based station to receive first ones of the software payloads, and wherein the inter-satellite communication portion communicates with at least one other satellite system to receive second ones of the software payloads.

4. The satellite system of claim 2, further comprising:

one or more sensor systems communicatively coupled with the virtualized execution system over associated communication links;

the virtualized execution system configured to provide access for ones of the virtual nodes to the one or more sensor systems as the resources of the satellite system.

5. The satellite system of claim 1, comprising:

the satellite control system configured to operate the logistical control elements of the satellite system independent of a state of the virtualized execution system, wherein the logistical control elements comprise one or more of satellite position control elements, satellite inertial control elements, satellite orbital control elements, satellite power control elements, and satellite thermal control elements.

6. The satellite system of claim 1, comprising:

the virtualized execution system comprising a hypervisor system configured to isolate execution and memory resources of the virtualized execution system among the ones of the software payloads when executing the associated virtual nodes; and

the virtualized execution system comprising a storage system configured to store at least the ones of the software payloads in an inactive state when not being executed by the virtualized execution system.

7. The satellite system of claim 1, comprising:

the communication interface configured to transfer the state information over at least an inter-satellite communication portion for delivery to at least the peer satellite system.

8. The satellite system of claim 1, further comprising:

one or more sensor systems communicatively coupled to the virtualized execution system, wherein the state information comprises data related to monitored sensor activity of the one or more sensor systems.

9. The satellite system of claim 1, comprising:

the virtualized execution system configured to receive peer state information related to execution of one or more virtual nodes on a further peer satellite system;

the virtualized execution system configured to establish execution of at least one virtual node on the satellite system in response to receiving the peer state information, the at least one virtual node continuing at least one activity performed by the further peer satellite system and indicated in the peer state information.

10. A method of operating a satellite system, the method comprising:

in a communication interface, receiving software payloads for execution by the satellite system;

in a satellite control system, operating logistical control elements of the satellite system; and

in a virtualized execution system, executing ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system, maintaining state information related to execution of ones of the virtual nodes, and transferring the state information over the communication interface for delivery to at least one peer satellite system configured as a backup to the satellite system.

11. The method of claim 10, further comprising:

in the virtualized execution system, executing the ones of the of software payloads as the associated virtual nodes on the satellite system according to at least a resource schedule that indicates timewise allocations of the associated virtual nodes to the resources of the satellite system.

12. The method of claim 11, further comprising:

in the communication interface, receiving the resource schedule over at least one of a ground communication portion and an inter-satellite communication portion, wherein the ground communication portion communicates with a ground-based station to receive first ones of the software payloads, and wherein the inter-satellite communication portion communicates with at least one other satellite system to receive second ones of the software payloads.

13. The method of claim 11, further comprising:

in the virtualized execution system, providing access for ones of the virtual nodes to one or more sensor systems as the resources of the satellite system according to at least the resource schedule, wherein the one or more sensor systems are communicatively coupled with the virtualized execution system over associated communication links.

14. The method of claim 10, further comprising:

in the satellite control system, operating the logistical control elements of the satellite system independent of a state of the virtualized execution system, wherein the logistical control elements comprise one or more of satellite position control elements, satellite inertial control elements, satellite orbital control elements, satellite power control elements, and satellite thermal control elements.

15. The method of claim 10, wherein the state information comprises data related to monitored sensor activity of one or more sensor systems communicatively coupled to the virtualized execution system.

16. The method of claim 10, further comprising:

in the communication interface, transferring the state information over at least an inter-satellite communication portion for delivery to the peer satellite system.

17. The method of claim 10, further comprising:

in the virtualized execution system, receiving peer state information related to execution of one or more virtual nodes on a further peer satellite system;

in the virtualized execution system, establishing execution of at least one virtual node on the satellite system in response to receiving the peer state information, wherein the at least one virtual node continues at least one activity performed by the further peer satellite system indicated in the peer state information.

18. A satellite software execution platform for a satellite system, comprising:

one or more computer readable storage media;

a processing system operatively coupled with the one or more non-transitory computer readable storage media; and

an execution service comprising program instructions stored on the one or more non-transitory computer readable storage media that, when read and executed by the processing system, direct the processing system to at least;

store software payloads for execution that are received over a communication interface comprising at least an inter-satellite communication portion;

execute ones of the software payloads deployed on the satellite system as associated virtual nodes, wherein the associated virtual nodes share resources of the satellite system.

19. The satellite software execution platform of claim 18, comprising further program instructions, when executed by the processing system, direct the processing system to at least:

provide access for ones of the virtual nodes to one or more sensor systems of the satellite system as the resources according to at least a resource schedule that indicates timewise allocation of the associated virtual nodes, wherein the one or more sensor systems are communicatively coupled with the execution service over associated communication links.

20. A satellite, comprising:

a communication interface configured to receive software payloads for execution by the satellite;

a satellite control system configured to operate logistical control elements of the satellite independent of a state of a virtualized execution system, wherein the logistical control elements comprise one or more of satellite position control elements, satellite inertial control elements, satellite orbital control elements, satellite power control elements, and satellite thermal control elements; and

the virtualized execution system configured to execute ones of the software payloads deployed on the satellite as associated virtual nodes that share resources of the satellite.

21. A method of operating a satellite, the method comprising:

in a communication interface, receiving software payloads for execution by the satellite;

in a satellite control system, operating logistical control elements of the satellite independent of a state of a virtualized execution system, wherein the logistical control elements comprise one or more of satellite position control elements, satellite inertial control elements, satellite orbital control elements, satellite power control elements, and satellite thermal control elements; and

in the virtualized execution system, executing ones of the software payloads deployed on the satellite as associated virtual nodes that share resources of the satellite.