Fms Autoflight
✈️ FMS Cooperation with Autoflight Systems
Big Picture
The FMS computes the flight path. The autoflight systems execute it.
FMS = brains (planning & guidance) Autoflight = muscles (flying the aircraft)
Systems Involved
Autoflight Systems
- Autopilot (AP) – flies pitch/roll
- Flight Director (FD) – gives guidance bars
- Autothrottle / Autothrust – controls thrust for speed or path
Data Link
Continuous exchange between:
- FMS computers
- Autoflight computers
- Displays (FMA on PFD)
How They Cooperate (Generic Flow)
Crew programs FMS
- Route, SID/STAR, constraints
- Weights, speeds, CI
FMS computes
- Lateral path (LNAV)
- Vertical path (VNAV)
- Speed targets
- Thrust requirements
Pilot selects modes
- Via MCP (Boeing) or FCU (Airbus)
Autoflight executes
- AP follows pitch/roll commands
- A/T or A/THR sets thrust
- FD shows guidance if AP off
Crew monitors
- FMA confirms who is controlling what
- Pilot intervenes if needed
Boeing Cooperation Logic
Boeing philosophy: Pilot commands
FMS provides targets and guidance
Pilot must:
- Set altitude, speed, heading in MCP
- Select LNAV / VNAV / FLCH
Autoflight follows MCP + FMS logic
Key point: 👉 The aircraft obeys the windows first, FMS second.
Example:
- VNAV active → FMC controls profile
- FLCH selected → FMC vertical path ignored
Airbus Cooperation Logic
Airbus philosophy: Pilot manages
FMS directly commands guidance
Pilot chooses:
- Managed (push) → FMGS controls
- Selected (pull) → pilot overrides
Autoflight closely integrated with FMGS
Key point: 👉 In managed modes, FMGS drives AP and A/THR directly.
Speed & Thrust Cooperation
Boeing
Autothrottle moves thrust levers
Speed from:
- MCP window or
- FMC (VNAV)
Airbus
- Autothrust active in detents
- Speed controlled electronically
- Thrust levers do not move
FMA — The Contract with the Pilot
On both aircraft, the Flight Mode Annunciator tells you:
- Who controls lateral
- Who controls vertical
- Who controls speed/thrust
👉 If it’s not on the FMA, it’s not happening.
Failure & Degradation Cooperation
Boeing
- Loss of FMS → revert to basic modes
- Pilot authority unchanged
Airbus
- Loss of FMGS or sensors → law degradation
- Managed modes lost, selected modes remain
Exam Summary Table
| Aspect | Boeing | Airbus |
|---|---|---|
| FMS role | Advisor + path computer | Manager + path controller |
| Pilot action | Set targets | Choose managed/selected |
| Autoflight | Follows MCP + FMS | Follows FMGS |
| Override | Immediate | Requires mode change |
| Key monitor | MCP + FMA | FMA (critical) |
The FMS computes the flight path, and the autoflight systems execute it; Boeing requires pilot-commanded targets, while Airbus allows the FMS to manage guidance directly in managed modes.