Common unmanned system architecture

Patent metadata

Field	Value
Publication number	US-11656670-B2
Application number	US-201816218428-A
Country	US
Kind code	B2
Filing date	Dec 12, 2018
Priority date	Dec 12, 2018
Publication date	May 23, 2023
Grant date	May 23, 2023

Abstract

Apparatus and methods for controlling unmanned systems (UMSs), such as unmanned aircraft, are provided. A UMS can include core systems, auxiliary systems, a payload, a physical computer, a network, and a power system. The network can enable the physical computer to communicate with the auxiliary systems using a second communications tier and with the payload using a third communications tier. The network and the physical computer can logically separate the second and third communications tiers. The power system can provide a first, second, and third power domains respectively for the core systems, the auxiliary systems, and for the payload. The power system can include circuitry that inhibits an overcurrent fault in the third power domain from causing an electrical fault in the first and second power domains and that inhibits an overcurrent fault in the second power domain from causing an electrical fault in the first power domain.

First claim

What is claimed is:

1. An unmanned system (UMS), comprising:
one or more core systems for the UMS;
one or more auxiliary systems for the UMS;
a payload;
a physical computer communicating with the one or more core systems for the UMS using a first tier of communications that provides a guaranteed bandwidth capability;
a network that enables the physical computer to communicate with the one or more auxiliary systems for the UMS using at least a second tier of communications, and communicate with the payload using a third tier of communications, wherein the network and the physical computer logically separate at least the second tier of communications and the third tier of communications, wherein the second tier of communications are isolatable from the third tier of communications and wherein the second tier of communications and the third tier of communications provide unguaranteed bandwidth;
a power system that provides a first power domain for the one or more core systems for the UMS and provides uninterruptible power for the first power domain, a second power domain for the one or more auxiliary systems for the UMS, and a third power domain for the payload,
wherein the power system provides interruptible power for each of the second power domain and the third power domain;
wherein each of the first tier of communications, the second tier of communications, and the third tier of communications is managed by a separate virtual computer and the virtual computer of the second tier of communications is configured to control the virtual computer of the third tier of communications, and wherein the power system signals a payload power off signal to the payload upon detection of the virtual computer for the second tier of communications being reset; and
the power system comprising first circuitry that inhibits a single overcurrent fault in the third power domain from causing an electrical fault in either the first power domain or the second power domain and second circuitry that inhibits a single overcurrent fault in the second power domain from causing an electrical fault in the first power domain.

2. The UMS of claim 1 , wherein the one or more core systems for the UMS comprise an autopilot and one or more servos for controlling one or more flight control surfaces of the UMS.

3. The UMS of claim 1 , wherein the physical computer comprises software that, when executed by the physical computer, causes the physical computer at least to perform functionality of a plurality of virtual computers.

4. The UMS of claim 3 , wherein the third tier of communications is associated with a third-tier network interface, and wherein the functionality of the plurality of virtual computers comprises:
virtualizing the third-tier network interface into a plurality of virtualized third-tier network interfaces, wherein the plurality of virtual computers are configured to utilize the plurality of virtualized third-tier network interfaces to communicate with the payload.

5. The UMS of claim 1 , wherein the network further enables the physical computer to communicate with the core systems for the UMS using a first tier of communications that comprises position and stability control messages.

6. The UMS of claim 1 , wherein the one or more auxiliary systems for the UMS comprise a remote control interface, and wherein the second tier of communications comprises UMS control messages communicated between the physical computer and the remote control interface.

7. The UMS of claim 1 , wherein the third tier of communications comprises payload control messages and payload data messages communicated between the physical computer and the payload.

8. The UMS of claim 7 , wherein the payload comprises one or more sensors, and wherein the payload data messages comprise data collected by the one or more sensors.

9. The UMS of claim 7 , wherein the payload comprises an imaging system, and wherein the payload data messages comprise one or more images and/or video imagery captured by the imaging system.

10. The UMS of claim 1 , wherein message traffic for both the second tier of communications and the third tier of communications is communicated using a single physical link of the network.

11. The UMS of claim 1 , wherein the network comprises a switching device configured to logically separate the second tier of communications and the third tier of communications by at least:
determining whether message traffic on the third tier of communications exceeds a third traffic threshold; and
after determining that message traffic on the third tier of communications exceeds a third traffic threshold, limiting message traffic on the third tier of communications to be less than the third traffic threshold.

12. The UMS of claim 11 , wherein the switching device is configured to logically separate the second tier of communications and the third tier of communications by at least:
blocking all message traffic from the second tier of communications, from the third tier of communications, or from both the second tier of communications and the third tier of communications.

13. The UMS of claim 1 , wherein the first power domain comprises a first power module, the second power domain comprises a second power module, and the third power domain comprises a third power module, wherein the third power module comprises the first circuitry, and wherein the second power module comprises the second circuitry.

14. The UMS of claim 13 , wherein the first power module comprises circuitry to provide a first set of functions that include a function for providing power and a function for sensing provided power.

15. The UMS of claim 14 , wherein the second power module comprises circuitry to provide a second set of functions that includes the first set of functions, a circuit breaking function, and a power on/off function.

16. The UMS of claim 15 , wherein the second power module comprises a circuit breaker configured to performing the circuit breaking function, and
wherein the second circuitry that inhibits a single overcurrent fault in the second power domain from causing an electrical fault in the first power domain comprises the circuit breaker.

17. The UMS of claim 15 , wherein the third power module comprises circuitry to provide a third set of functions that include the second set of functions and a function for powering down the payload in response to a power fault.

18. The UMS of claim 17 , wherein each of the first power module, the second power module and the third power module comprises a mode indicator to select between the first set of functions, the second set of functions, and the third set of functions,
wherein the mode indicator for the first power module is set to select the first set of functions,
wherein the mode indicator for the second power module is set to select the second set of functions, and
wherein the mode indicator for the third power module is set to select the third set of functions.

19. The UMS of claim 1 , wherein the network comprises an input/output node configured to communicate with the physical computer using a packet-based interface and to receive inputs and provide outputs from a plurality of input/output devices via a plurality of communications protocols.

20. The UMS of claim 1 , wherein the power system signals a payload power off signal to the payload upon detection of one or more of the following conditions: an overcurrent condition for electrical power provided by a propulsion module of the UMS, and an overcurrent condition for ele

Assignees

• Insitu Inc

Inventors

• Rathbun David
• Miller Douglas Allyn
• Hillen Kenneth
• Fix Brian

Classifications

• B64U50/30

  Supply or distribution of electrical power · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64U10/25

  Fixed-wing aircraft (VTOL aircraft B64U10/20) · CPC title

• Y02T50/40

  Weight reduction · CPC title

• G06F9/45558 Primary

  Hypervisor-specific management and integration aspects · CPC title