Control Laws Flashcards

1
Q

Control laws and their characteristics

A

• Normal law

  • Pitch: Vertical load factor
  • Bank: Roll rate

• Alternate law

  • Pitch: Vertical load factor
  • Bank: Roll rate in ALTN1 / Direct control of ailerons in ALTN2
  • Direct law, direct relationship between stick and flight control surfaces
  • Ground law (before lift-off and after touch-down), same as Direct law
  • Flare law (allow conventional flare):
  • Pitch: Stick orders a pitch attitude increment to a reference attitude
  • Bank: Direct control of ailerons
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2
Q

Protections in normal law

A
  • Load factor protection
  • High speed protection
  • High angle-of-attack protection
  • Pitch attitude protection
  • Bank angle protection
  • Low energy warning
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3
Q

Protections in alternate law

A

• Load factor protection
• Bank angle protection (ALTN1 only)
• Low speed stability:
- VSW replaces αPROT and αMAX
- If speed reduces to VSW, AP disconnect and a nose down pitch input is introduced
• High speed stability:
- Amber dashes replace the Green dashes on speed scale
- If speed increases to VMO, AP disconnect and a nose up pitch input is introduced
• Aural stall
• Overspeed warning

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4
Q

Protections in Alternate law without stability

A
  • Load factor protection
  • Aural stall
  • Overspeed warning
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5
Q

Load factor protection

A

• Load factor limitation:
+ 2.5 g, -1 g in clean configuration
+ 2 g, 0 g when slats are extended

• Rapid pull-up to 2.5 g is immediately possible.

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6
Q

High speed protection

A

• VMO + 4 kt / MMO+ 0.006,
Overspeed Ecam warning

• VMO +6 kt / MMO + 0.01, Automatic pitch up applied

• VMO + 16 kt / MMO +0.04,
Maximum stabilized speed stick maintained nose down

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7
Q

High angle-of-attack protection

A
  • VLS: Minimum allowed speed, A/THR in speed mode will not allow speed to drop below VLS even if lower speed is selected
  • Vα Prot: AP disengages, Auto Pitch trim stops
  • Vα Floor: TOGA thrust is set automatically
  • Vα Max: Speed is maintained with full aft stick, speed brake retract if previously extended
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8
Q

Pitch attitude protection

A

• Nose-down, 15°
• Nose-up,
- 30° in conf 0 to 3 reduced to 25° at low speed
- 25° in conf FULL reduced to 20° at low speed

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9
Q

Bank angle protection

A

• Bank angle limited to 67°
• Above 33°:
- Stick released, aircraft rolls back to 33°
- Stick maintained, bank angle maintained
• In high speed protection:
- Spiral stability is introduced regardless of angle
- bank angle is limited to 40°
• In high angle-of-attack protection, bank angle is limited to 45°

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10
Q

Low energy warning

Available between 100 ft and 2000 ft RA in Conf 2, 3 and Full

A
  • Aural warning, “SPEED SPEED SPEED”

* To stop the warning, increase Thrust

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11
Q

Protections in Direct law

A
  • Aural stall

* Overspeed warning

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