Comprehensive Study Guide_ Automatic Flight Control Systems (AFCS) PDF
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This document provides a comprehensive study guide on Automatic Flight Control Systems (AFCS). It details the concepts of Flight Director, Autopilot (AP), and Auto Throttle (AT). Covers their functions, components, modes, and operational phases. Also includes information on Yaw Damper operations and integration with autopilot systems.
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Comprehensive Study Guide: Automatic Flight Control Systems (AFCS) Objectives Flight Director (FD): Understand its purpose, components, inputs, and modes of operation. Autopilot: Explore its functionality, control mechanisms, and various operational modes. Auto Thro...
Comprehensive Study Guide: Automatic Flight Control Systems (AFCS) Objectives Flight Director (FD): Understand its purpose, components, inputs, and modes of operation. Autopilot: Explore its functionality, control mechanisms, and various operational modes. Auto Throttle: Learn its purpose, operational phases, and integration into flight management. Yaw Damper: Examine its role in maintaining directional stability and damping Dutch Roll oscillations. Flight Director (FD) Purpose: Assists pilots by providing pitch and roll steering commands to maintain a desired flight path, displayed on the ADI. These commands ensure smooth changes in altitude and heading. Inputs and Computations: ○ Inputs include ADC, compass systems, vertical gyros, and VHF navigation radios. ○ Computed by two main systems: Roll Computer (lateral steering) and Pitch Computer (vertical steering). Modes: ○ Heading, VOR/LOC, Approach (auto/manual), Altitude Hold, Go-Around, and Back Course. ○ Specific functions, such as VOR/LOC, use inputs like course deviation and roll attitude to adjust commands. Displays: ○ V-Bar Display: Combines pitch and roll commands into an integrated cue. ○ Split-Cue Display: Displays independent left/right and up/down commands using crosshairs. Key Features: ○ Commands are limited (±12° pitch, varying roll limits by mode: ±30° Heading, ±25° VOR/LOC, ±15° Approach). ○ Gain programming adjusts command sensitivity, especially during narrow glideslope beam approaches. Autopilot (AP) Function: Electronically controls pitch, roll, and yaw, reducing pilot workload. Capable of precision tasks such as automatic landing in modern systems. Operational Modes: ○ Control Wheel Steering (CWS): Pilot manually inputs commands, processed to assist flight control. ○ Command Mode: Fully automated based on AFCS Mode Control Panel inputs like heading and altitude. Components and Systems: ○ Roll Channel: Manages ailerons and spoilers, with outputs converted to mechanical movements via PCU. ○ Pitch Channel: Controls elevators and stabilizers; retrims stabilizers automatically for sustained pitch changes. ○ Yaw Channel: Uses the rudder for yaw damping and turn coordination. Servo Systems: ○ Electro-pneumatic: Simpler systems for direct control. ○ Electro-mechanical and hydraulic: Used in advanced aircraft for precision and redundancy. Advanced Functions: ○ Glideslope deviation attenuation ensures smooth transitions during ILS approaches. ○ Integration with sensors like Low Range Radio Altimeter for altitude precision. Auto Throttle (AT) Purpose: Automates throttle management to maintain thrust and speed parameters, reducing workload. Operational Phases: ○ Takeoff: Automatically sets N1 thrust based on environmental factors. ○ Climb and Cruise: Adjusts to meet speed or Mach requirements, optimizing fuel efficiency. ○ Descent: Maintains idle thrust while observing speed limits. ○ Go-Around: Rapidly increases thrust to achieve required climb rates. ○ Flare: Retards throttles for landing. Key Components: ○ Servo actuators, torque sensing mechanisms, and override systems for manual control. ○ Power Lever Angle (PLA) synchros ensure feedback on throttle positions. Yaw Damper Purpose: Stabilizes directional oscillations (Dutch Roll), especially in swept-wing aircraft prone to dihedral effects. Operation: ○ Utilizes rate gyros to detect oscillations and dampens them via rudder deflections. ○ Controlled by a yaw damper computer, working through hydraulic PCUs. ○ Operates independently of pilot inputs, with no feedback to rudder pedals. Key Features: ○ Limited rudder movement (2–5°) based on airspeed and aerodynamic requirements. ○ Gain programming modifies response sensitivity depending on flight conditions. Types: Series yaw damping integrates with pilot rudder inputs for coordinated turns. Flight Director and Autopilot Integration Modes and Functions: ○ Heading Mode: Guides aircraft to a preselected heading using roll adjustments. ○ VOR/LOC Mode: Tracks VOR radials or localizer courses, transitioning to ILS approaches when necessary. ○ Approach Mode: Combines localizer and glideslope capture, ensuring precision landing. ○ Altitude Modes: Altitude Hold maintains barometric levels; Preselect sets desired levels; Vertical Speed adjusts climb/descent rates. Beam Capture: Smoothly transitions to track VOR or localizer beams, arming for glideslope capture during approaches. Safety Enhancements: Disengagement protocols include visual and auditory alerts, ensuring pilot awareness. Key Components and Sensors Inputs: ○ Vertical: VG, AHRS, IRU, ADC provide altitude and attitude data. ○ Lateral: Gyros, compass systems, and VHF navigation ensure directional accuracy. Actuation: ○ Servo motors or hydraulic PCUs translate computed commands into physical control surface adjustments. ○ Feedback loops stabilize aircraft by nullifying error signals. Integrated Protections: Flight envelope safeguards prevent overstressing the aircraft during operations. Summary of FD Commands Displays: Combines pitch and roll guidance for intuitive adjustments during all flight phases. Modes: Supports diverse scenarios, including Back Course approaches and Go-Around maneuvers. Error Correction: Steering commands dynamically address deviations from the flight path. Autopilot Operational Enhancements Detailed Logic: Advanced interlock systems ensure reliable engagement and safe operation. Specialized Modes: ○ Turbulence Mode: Improves response during unstable weather conditions. ○ Altitude Select: Precisely transitions to target altitudes, supported by CADC inputs. Safety Features: ○ Disengagement alerts, such as flashing panel lights and control column warnings, maintain pilot situational awareness. ○ Override mechanisms allow manual control in emergencies. This enhanced study guide now incorporates deeper technical details and additional operational examples, ensuring a robust resource for exam preparation.