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  2. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    A control system includes control surfaces which, when deflected, generate a moment (or couple from ailerons) about the cg which rotates the aircraft in pitch, roll, and yaw. For example, a pitching moment comes from a force applied at a distance forward or aft of the cg, causing the aircraft to pitch up or down.

  3. Flight control modes - Wikipedia

    en.wikipedia.org/wiki/Flight_control_modes

    A flight control mode or flight control law is a computer software algorithm that transforms the movement of the yoke or joystick, made by an aircraft pilot, into movements of the aircraft control surfaces. The control surface movements depend on which of several modes the flight computer is in.

  4. Sylver vertical launching system - Wikipedia

    en.wikipedia.org/wiki/Sylver_Vertical_Launching...

    K-VLS - A vertical launching system of Republic of Korea Navy. Mark 41 Vertical Launching System - A vertical launching system of United States Navy. Poliment-Redut - A vertical launching system of Russian Navy, navalized version of S-350. 3S-14 - A vertical launching system of Russian Navy for cruise, anti-ship and anti-submarine missiles.

  5. Roll program - Wikipedia

    en.wikipedia.org/wiki/Roll_program

    A roll program or tilt maneuver is an aerodynamic maneuver that alters the attitude of a vertically launched space launch vehicle. It consists of a partial rotation around the vehicle's vertical axis, allowing the vehicle to then pitch to follow the proper azimuth toward orbit. [1] A roll program is usually completed after the vehicle clears ...

  6. Horizontal takeoff and landing - Wikipedia

    en.wikipedia.org/wiki/Takeoff_and_landing

    Vertical takeoff, horizontal landing (VTHL) is the mode of operation for all current and formerly operational orbital spaceplanes, such as the Boeing X-37, the NASA Space Shuttle, the 1988 Soviet Buran space shuttle, and the PRC Reusable experimental spacecraft/Shenlong. For launch vehicles an advantage of VTHL over HTHL is that the wing can be ...

  7. Propeller synchronization - Wikipedia

    en.wikipedia.org/wiki/Propeller_synchronization

    The prop sync adjusts the r.p.m. of the “secondary” engine to precisely match the r.p.m. of the “primary” engine, and then maintains that relationship. The prop sync should be disengaged when the pilot selects a new propeller r.p.m., then re-engaged after the new r.p.m. is set.

  8. Spacecraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_flight_dynamics

    The control torque for a launch vehicle is sometimes provided aerodynamically by movable fins, and usually by mounting the engines on gimbals to vector the thrust around the center of mass. Torque is frequently applied to spacecraft, operating absent aerodynamic forces, by a reaction control system, a set of thrusters located about the vehicle ...

  9. Vertical navigation - Wikipedia

    en.wikipedia.org/wiki/Vertical_navigation

    In aviation, vertical navigation (VNAV, usually pronounced vee-nav) is glidepath information provided during an instrument approach, independently of ground-based navigation aids in the context of an approach and a form of vertical guidance in the context of climb/descent. An onboard navigation system displays a constant rate descent path to ...