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FDR_5_2_07_rev3
FDR_5_2_07_rev3

... • The state of a spacecraft can be described by a vector of 6 orbital elements. – Semi-major axis, a – Eccentricity, e – Inclination, i – Right ascension of the ascending node, Ω – Argument of perihelion, ω ...
Autonomous Flight
Autonomous Flight

Physiology of Flight
Physiology of Flight

also available online
also available online

... For simplicity, this review will assume circular orbits. Tethers can be in an ellipse; those are just more complicated to discuss. The two connected objects will move at the orbital velocity of their center of mass. If they have unequal masses, the lighter end will be farther from that center of mas ...
interstellar precursor mission - Colorado Space Grant Consortium
interstellar precursor mission - Colorado Space Grant Consortium

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09_Final_Flight_Club - Colorado Space Grant Consortium
09_Final_Flight_Club - Colorado Space Grant Consortium

... The advice Team Flight Club would give to next year’s teams would be to figure out what you want your scientific experiment to be as early as possible. It can be a bit daunting given a blank slate, but try to come up with the general focus of your experiment before doing anything else. Also, it’s ni ...
X-33 - blackboard TU Delft
X-33 - blackboard TU Delft

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In Our Galaxy, Far, Far Away

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Aerodynamics
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Meet the Planets - Arbordale Publishing
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Cool Jobs: Exploring the solar system | Science News for Students

... visited, could help explain how our solar system formed. People have been studying the sun and planets for thousands of years. Scientists, though, still have many questions about Earth’s neighborhood. They search for clues about what the solar system looked like in its earliest days, how planets wer ...
The Aerodynamic Forces code grew steadily over the course of the
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... the first spacecraft to pass through the asteroid belt and the first to obtain close-up images of Jupiter. In 1983, it became the first manmade object to leave the Solar System when it passed the orbit of Pluto. The Pioneer 10 spacecraft, destined to be the first man-made object to escape our solar ...
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Smart avionics for the Cessna CJ1+/CJ2+
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... workload-reducing automation on the flight deck with true multi-sensor navigation capability. The result – seamless takeoff-to-touchdown flight guidance, direct-to-anywhere simplicity and significantly improved eyes-up display capability for the CJ1+/CJ2+. Used in conjunction with the GPS-4000S WAAS ...
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CDIO S S P D
CDIO S S P D

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Flight dynamics (spacecraft)



Spacecraft flight dynamics is the science of space vehicle performance, stability, and control. It requires analysis of the six degrees of freedom of the vehicle's flight, which are similar to those of aircraft: translation in three dimensional axes; and its orientation about the vehicle's center of mass in these axes, known as pitch, roll and yaw, with respect to a defined frame of reference.Dynamics is the modeling of the changing position and orientation of a vehicle, in response to external forces acting on the body. For a spacecraft, these forces are of three types: propulsive force (usually provided by the vehicle's engine thrust); gravitational force exerted by the Earth or other celestial bodies; and aerodynamic lift and drag (when flying in the atmosphere of the Earth or other body, such as Mars or Venus). The vehicle's attitude must be taken into account because of its effect on the aerodynamic and propulsive forces. 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 principles of flight dynamics are normally used to control a spacecraft by means of an inertial navigation system in conjunction with an attitude control system. Together, they create a subsystem of the spacecraft bus often called ADCS.
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