Advanced air data system architecture with air data computer incorporating enhanced compensation functionality

A system comprising:

• a first air data system configured to provide first air data parameters;
• a second air data system configured to provide second air data parameters;
• a third air data system configured to provide third air data parameters, wherein each of the first, second, and third air data systems comprise:
• an air data computer (ADC) comprising a single pneumatic port for receiving a pneumatic input, a plurality of electrical inputs for receiving one or more electrical signals, and an output;
• a pitot pressure probe discrete from the ADC configured to sense pitot pressure of the oncoming airflow about an aircraft exterior, wherein the pitot pressure probe is pneumatically coupled to the single pneumatic port of the ADC;
• a first static pressure probe configured to be aligned with the aircraft exterior to sense static pressure of the oncoming airflow about the aircraft exterior;
• and
• a second static pressure probe configured to be mounted parallel to the aircraft exterior to sense static pressure of the oncoming airflow about the aircraft exterior, wherein each ADC of the first, second, and third air data systems is configured transmit, via respective outputs, first, second, and third air data parameters, respectively, based on the pneumatic input and the one or more electrical signals received by respective ADCs;
• a standby instrument;
• a first standby pressure module pneumatically coupled to the pitot pressure probe of the first air data system and configured to transmit a first standby pressure signal representative of pitot pressure of the oncoming airflow about the aircraft exterior to the standby instrument;
• a second standby pressure module pneumatically coupled to the first static pressure probe of the first air data system and configured to transmit a second standby pressure signal representative of static pressure of the oncoming airflow sensed by the first static pressure probe of the first air data system;
• and
• a third standby pressure module pneumatically coupled to the second static pressure probe of the third air data system and configured to transmit a third standby pressure signal representative of static pressure of the oncoming airflow sensed by the second static pressure probe of the third air data system.