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Normal Law


Operates in 3 modes:

  • ground mode, when on the ground and controls are conventional (direct law)
  • flight mode, in the air after a gradual transition from ground mode
  • flare mode, the introduction of a conventional feel to the landing phase passing 100' (direct law)

Side stick deflection gives a rate demand to the flight control computers. The demand is rate of roll in roll, and load factor (g) in pitch. Rudder pedal inputs are not required for turn coordination or dutch roll damping.


Control

Normal Law
Pitchgrounddirect
flightload factor
flaredirect
Rollgroundproportional
flightroll rate
flareroll rate

Protections

NameAxisDescription
Load factor limitationverticallimits maximum g loads: +2.5g to -1g (clean), +2g to 0g
Pitch attitudeverticallimits pitch: 25° to 30° NU, 15° ND
High angle of attackverticalhas priority over other protections, limits based on airspeed: VLS (with autothrust), VαPROT (no autothrust), VαMAX (overridden with side stick)
between αPROT and αMAX, AOA is proportional to side stick and returns to αPROT if released
High speedverticallimits airspeed: slightly >VMO/MMO
Bank anglelaterallimits bank angle: 67°, 33° when side stick released, 45° limit with high speed or angle of attack protection

/wiki/wikis/a330/bin/alpha.jpg/wiki/wikis/a330/bin/alpha2.jpg
Figure: VLS, VαPROT, VαMAXFigure: High angle of attack protection airspeed tape indications

Turbulence damping function

Damps structural modes induced by turbulence. It may be manually inhibited using the TURB DAMP pb sw.


Failures

A single failure cannot result in loss of normal law, however multiple failures of flight control, hydraulics, or electrical systems may result in a degradation of the flight control law.


Reconfiguration Control Laws: Normal Law → Alternate Law (1 and 2)Direct LawMechanical Backup


F/CTL ALTN LAW (PROT LOST)- degradation to alternate law
F/CTL DIRECT LAW (PROT LOST)- degradation to direct law

Categories: Airbus A330 | Flight Controls



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