Methods and systems for advanced spaceport information management

A method of testing a payload, comprising:

• coupling a test system to the payload;
• transmitting one or more test signals that at least one of emulate and enable an anticipated condition from the test system to the payload;
• receiving one or more responsive signals from the payload into the test system;
• analyzing one or more responsive signals;
• and
• determining whether one or more of the responsive signals comprises an anomalous signal,
• wherein at least one of the transmitting one or more test signals, receiving one or more responsive signals, analyzing one or more responsive signals, and determining whether one or more of the responsive signals comprises an anomalous signal includes transmitting at least one of the test signals and the responsive signals via a communications link from a payload processing facility to a remotely located facility.

A computer-readable medium having stored thereon instructions for testing a payload, the computer-readable medium comprising:

• a first computer program portion adapted to transmit one or more test signals that emulate an anticipated condition from a test system to the payload;
• a second computer program portion adapted to receive one or more responsive signals from the payload into the test system;
• a third computer program portion adapted to analyze one or more responsive signals;
• and
• a fourth computer program portion adapted to determine whether one or more of the responsive signals comprises an anomalous signal,
• wherein at least one of the first, second, third, and fourth computer program portions is further adapted to communicate via a communications link from a payload processing facility to a remotely located facility.

An avionics software tasking model for testing a payload, comprising:

• a hardware driver layer;
• and
• a payload test system operatively coupled to the hardware driver layer, the payload test system including:
• a front end adapted to be operatively coupled to and communicate with the payload;
• a back end operatively coupled to the front end;
• and
• a payload data repository operatively coupled to at least one of the back end and the front end,
• wherein at least one of the operative couplings between the front end and the payload, and the back end and the front end, and the payload data repository and the at least one of the back end and the front end is adapted to include a communications link from a payload processing facility to a remotely located facility.

A payload life cycle, comprising:

• a preflight operations portion that includes a payload test procedure, the payload test procedure including:
• transmitting one or more test signals that emulate an anticipated condition from a test system to the payload;
• receiving one or more responsive signals from the payload into the test system;
• analyzing one or more responsive signals;
• and
• determining whether one or more of the responsive signals comprises an anomalous signal,
• wherein at least one of the transmitting, receiving, analyzing, and determining comprises communicating via a communications link from a payload processing facility to a remotely located facility;
• a flight system integration portion that includes integration of the payload within a launch vehicle;
• and
• a desired mission portion.

A data management architecture adapted for testing a payload, comprising:

• a common infrastructure adapted to perform at least one core function;
• one or more modules operatively interfaced with the common infrastructure, the one or more modules including at least one of:
• an input module adapted to receive input data;
• a test script generation module adapted to generate a test script for testing the payload;
• and
• an integration simulator module adapted to provide simulation data to the payload;
• and
• a communications link operatively coupled to at least one of the common infrastructure and the one or more modules, the communications link being adapted to enable a payload developer at a remotely located facility to autonomously perform a payload test procedure of the payload.