Aircraft: LCA, HAL-Tejas
source ==> inputs ==> algorithm ==> outputs ==> destination
Air Data Probe - pitot tube, static port - 3 (nose, left, right)
TAT sensor - 1 (down)
AOA sensor - 2 (left, right)
AOSS Sensor - 2 (left, right)
https://www.indiatoday.in/india/story/watch-video-iaf-chief-rks-bhaduria-tejas-fighter-lca-squadron-sulur-1682403-2020-05-27
Air Data Computer ADC - 4 (RS-422) ==> ADC1, ADC2, ADC3, ADC4
other avionics systems: MIL-STD-1553B
processor: intel i960 (80960) - 32-bit processor
source code: Ada language
testing, for expected output: C language
testing, for test procedure: Ada language
outputs:
airspeed - IAS, CAS, EAS, TAS, Mach number, VS
altitude – uncorrected pressure altitude, baro corrected pressure altitude,
pressures data - static pressure, dynamic pressure, total pressure
temperatures data - TAT, SAT, International Standard Atmosphere (ISA) delta temperature
AOA - Angle of attack (relative wind and chordline of wing)
AOSS - Angle of side slip (relative wind and longitudinal axis)
VMO/MMO (max operational airspeed / max operational Mach)
ADS sends date to:
pilot - display system
flight control system
flight management system
engine control systems