Aircraft Recording System Interface for Rapid Configuration
Aircraft recording system configuration devices and methods are disclosed. The systems and methods provide a context-sensitive interface for rapid configuration. An aircraft recording system is operatively coupled to a data collection interface that is powered off and in an unconfigured state upon an initial installation of the aircraft recording system configuration device onboard an aircraft. A physical interface is disposed on an outer surface of the aircraft recording system configuration device, such that activating the physical interface causes an initial configuration of the aircraft recording system to be established. An indicator is further provided that disposed on the outer surface of the aircraft recording system configuration device, wherein the indicator is configured to indicate different states of the aircraft recording system.
1 . An aircraft recording system configuration device having a context-sensitive interface for rapid configuration, the aircraft recording system configuration device comprising:
an aircraft recording system interface operatively coupled to an aircraft recording system by way of a data collection interface, wherein upon initial installation of the aircraft recording system configuration device onboard an aircraft, the aircraft recording system is powered off and in an initial state;
a physical interface disposed on an outer surface of the aircraft recording system configuration device, wherein activating the physical interface causes an initial configuration of the aircraft recording system to be established; and
an indicator associated with the aircraft recording system configuration device, wherein the indicator is configured to indicate different states of the aircraft recording system.
2 . The aircraft recording system configuration device of claim 1 , wherein the initial state is an unconfigured state.
3 . The aircraft recording system configuration device of claim 1 , wherein the initial state is a configured state that is operative to transition from the configured state to an unconfigured state by way of receiving an instruction to enter a reset state.
4 . The aircraft recording system configuration device of claim 1 , wherein the indicator comprises a power indicator and a fault indicator.
5 . The aircraft recording system configuration device of claim 1 , wherein the data collection interface is coupled with an ethernet connectivity pathway that enables data to be multiplexed from the data collection interface to the aircraft recording system.
6 . The aircraft recording system configuration device of claim 1 , wherein the indicator is disposed on the outer surface of the aircraft recording system configuration device.
7 . The aircraft recording system configuration device of claim 1 , wherein the physical interface is integrated into the aircraft recording system configuration device.
8 . A configuration method for configuring an aircraft recording system using an aircraft recording system configuration device, the configuration method comprising:
providing the aircraft recording system configuration device, wherein the aircraft recording system configuration device is unpowered and in an initial state of configuration;
powering the aircraft recording system configuration device by activating a physical interface disposed on an outer surface of the aircraft recording system configuration device, wherein the physical interface comprises an indicator;
automatically configuring the aircraft recording system into a default configuration state using the aircraft recording system configuration device; and
recording aircraft data via the aircraft recording system by way of a data collection interface.
9 . The configuration method of claim 8 , wherein the initial state of configuration is an unconfigured state.
10 . The configuration method of claim 8 , wherein the initial state of configuration is a configured state that is operative to transition from the configured state to the default state by way of receiving an instruction to enter the default state.
11 . The configuration method of claim 8 , wherein the indicator comprises a power indicator and a fault indicator.
12 . The configuration method of claim 8 , wherein the data collection interface is coupled with an ethernet connectivity pathway that enables data to be multiplexed from the data collection interface to the aircraft recording system.
13 . The configuration method of claim 8 , wherein the indicator is disposed on the outer surface of the aircraft recording system configuration device.
14 . The configuration method of claim 8 , wherein the physical interface is integrated into the aircraft recording system configuration device.
15 . A configuration method for configuring an aircraft recording system, the configuration method comprising:
providing an aircraft recording system configuration device, wherein the aircraft recording system configuration device is unpowered and in an initial state of configuration;
powering the aircraft recording system configuration device by activating a physical interface disposed on an outer surface of the aircraft recording system configuration device;
booting a wireless interface;
wirelessly connecting to an external device;
uploading a configuration file to the aircraft recording system configuration device from the external device;
establishing a configuration state via the configuration file; and
recording aircraft data via the aircraft recording system.
16 . The configuration method of claim 15 , wherein the initial state of configuration is an unconfigured state.
17 . The configuration method of claim 15 , wherein the initial state of configuration is a configured state that is operative to transition from the configured state to a default state by way of receiving an instruction to enter the default state.
18 . The configuration method of claim 15 , wherein an indicator associated with the aircraft recording system comprises a power indicator and a fault indicator.
19 . The configuration method of claim 18 , wherein the indicator is disposed on the outer surface of the aircraft recording system configuration device.
20 . The configuration method of claim 15 , wherein the physical interface is integrated into the aircraft recording system configuration device.