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Flight management system

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A flight management system (FMS) is a vital component of modern airliner avionics.

Honeywell FMS
Honeywell FMS

It is a specialized computer system designed to automate many in-flight tasks. This automation reduces the workload on flight crews significantly. Because of the FMS, modern civilian aircraft no longer require dedicated flight engineers or navigators. The system essentially acts as the brain for navigating and managing the aircraft's journey. It ensures the plane follows a precise path while optimizing how it flies.

The FMS operates as a dual system. It consists of the flight management computer (FMC), a control display unit (CDU), and a cross talk bus. The CDU is the interface used by pilots in the cockpit. It usually features a small screen and a keyboard or a touchscreen. Once the pilots enter data, the FMS sends the flight plan to various cockpit displays. These include the electronic flight instrument system (EFIS), the navigation display (ND), or the multifunction display (MFD). On these screens, the flight plan typically appears as a bright magenta line.

To function, the FMS relies on a navigation database (NDB). This database contains the essential elements needed to construct a flight plan. These elements are defined by the ARINC 424 standard. The NDB includes waypoints, intersections, airways, and airports. It also contains data for runways and radio navigation aids. These aids include distance measuring equipment (DME), VHF omnidirectional range (VOR), non-directional beacons (NDBs), and instrument landing systems (ILSs). To keep this information current, the database is updated every 28 days. This cycle ensures that pilots are always using the most recent aeronautical data.

A primary task of the FMS is obtaining a position fix. This means determining exactly where the aircraft is located. The system uses several sensors to validate this position. High-quality GPS receivers serve as the primary sensor due to their high accuracy. The system also uses radio aids like VORs and Scanning DME. A Scanning DME can check distances from five different stations every 10 seconds. Additionally, an inertial reference system (IRS) uses ring laser gyros and accelerometers to calculate position. The IRS is highly accurate because it is independent of outside signals. Many airliners use a "triple mixed IRS" by taking a weighted average of three independent systems.

The FMS uses these inputs to calculate the course to follow. This guidance is divided into lateral and vertical components. Lateral Navigation (LNAV) provides roll steering commands to the autopilot to follow the side-to-side path. Vertical Navigation (VNAV) manages the aircraft's altitude, speed, and pitch. VNAV is highly sophisticated in large aircraft like the Airbus A320 or Boeing 737. It uses a comprehensive flight and engine model provided by the manufacturer. This model allows the FMS to predict the most efficient vertical path based on the aircraft's weight and fuel.

VNAV is essential for fuel efficiency and performance optimization. As an aircraft burns fuel, it becomes lighter and can fly higher to reduce drag. The FMS can manage "step climbs" or "cruise climbs" to take advantage of this. It also calculates the ECON speed, which is the most economical speed for level flight. This speed is determined by a cost index. The cost index is a ratio of the hourly operating cost of the plane to the cost of fuel. A cost index of zero focuses on maximum fuel economy, while a cost index of 999 prioritizes speed above all else.

The descent phase is also managed with great precision. The FMS calculates the top of descent (TOD) point. This is the location where an efficient descent should begin. To find this, the FMS "flies" the descent backward from the touchdown point. It considers the flight plan, the aircraft model, and the predicted descent winds. During this descent, the FMS often commands the throttles to an idle setting. This is known as an idle descent or a "green descent." This method uses minimum fuel and reduces both pollution and local noise. While very efficient, air traffic control often limits these descents to manage many aircraft at once.

The history of the FMS shows a path of increasing automation. The modern FMS was first introduced on the Boeing 767. Before this, earlier versions of navigation computers existed, but they were less integrated. Today, FMS technology has evolved so much that similar systems exist on small aircraft like the Cessna 182. From managing complex search patterns to calculating air release points for parachute jumps, the FMS has become a fundamental tool in aviation. It connects sensor data, mathematical models, and pilot input into a single, cohesive system for flight.

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File:Honeywell FMS.jpg
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