- Modern flight dynamics. (1961 edition) | Open Library
- David Schmidt-Modern Flight Dynamics-McGraw-Hill Science_Engineering_Math (2011) - ERRATA | Matrix (Mathematics) | Mathematical Concepts
- Modern Flight Dynamics: Schmidt, David: 9780073398112: Amazon.com: Books
- Flight dynamics - Wikipedia
The equilibrium roll angle is known as wings level or zero bank angle, equivalent to a level heeling angle on a ship. Yaw is known as "heading". A fixed-wing aircraft increases or decreases the lift generated by the wings when it pitches nose up or down by increasing or decreasing the angle of attack (AOA). The roll angle is also known as bank angle on a fixed-wing aircraft, which usually "banks" to change the horizontal direction of flight. An aircraft is streamlined from nose to tail to reduce drag making it advantageous to keep the sideslip angle near zero, though aircraft are deliberately "side-slipped" when landing in a cross-wind, as explained in slip (aerodynamics). Spacecraft and satellites [ edit] Propulsive, aerodynamic, and gravitational force vectors acting on a space vehicle during launch The forces acting on space vehicles are of three types: propulsive force (usually provided by the vehicle's engine thrust); gravitational force exerted by the Earth and other celestial bodies; and aerodynamic lift and drag (when flying in the atmosphere of the Earth or another body, such as Mars or Venus).
Modern flight dynamics. (1961 edition) | Open Library
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David Schmidt-Modern Flight Dynamics-McGraw-Hill Science_Engineering_Math (2011) - ERRATA | Matrix (Mathematics) | Mathematical Concepts
The vehicle's attitude must be controlled during powered atmospheric flight because of its effect on the aerodynamic and propulsive forces. [3] There are other reasons, unrelated to flight dynamics, for controlling the vehicle's attitude in non-powered flight (e. g., thermal control, solar power generation, communications, or astronomical observation). The flight dynamics of spacecraft differ from those of aircraft in that the aerodynamic forces are of very small, or vanishingly small effect for most of the vehicle's flight, and cannot be used for attitude control during that time. Also, most of a spacecraft's flight time is usually unpowered, leaving gravity as the dominant force.
Modern Flight Dynamics: Schmidt, David: 9780073398112: Amazon.com: Books
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- Modern Flight Dynamics: Schmidt, David: 9780073398112: Amazon.com: Books
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Flight dynamics - Wikipedia
