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Alternate Law

Also from: Altn Law


Ground and flare mode are the same as in normal law. In flight mode:

  • pitch control - unchanged
  • roll control - surface deflection is proportional to side stick deflection (like a conventional control)
  • yaw control - damping is available with limited authority

Control

ALT 1ALT 2
Pitchgrounddirectdirect
flightload factorload factor
flaredirectdirect
Rollgroundproportionaldirect
flightroll ratedirect
flareroll ratedirect

Protections

The following protections are lost or changed.


ALT 1ALT 2
load factor/wiki/wikis/a330/bin/tick.jpg/wiki/wikis/a330/bin/tick.jpg
pitch attitude/wiki/wikis/a330/bin/cross.jpg/wiki/wikis/a330/bin/cross.jpg
high angle of attacklow speed stabilitylow speed stability, or /wiki/wikis/a330/bin/cross.jpg if 2 × ADR failure
high speed protectionhigh speed stabilityhigh speed stability, or /wiki/wikis/a330/bin/cross.jpg if 3 × ADR failure
bank angle/wiki/wikis/a330/bin/tick.jpg/wiki/wikis/a330/bin/cross.jpg

Note that, according to failures, the above protections may not be available, leaving only load factor limitation protection.


NameAxisDescription
Low speed stabilityverticallimits speed loss: at VSW a nose down input is introduced (can be overridden by the stick)
High speed stabilityverticallimits high speed: above VMO/MMO nose up input is introduced (can be overridden by the stick)

Categories: Airbus A330 | Flight Controls



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