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A spacecraft's attitude must typically be stabilized and controlled for a variety of reasons. It is often needed so that the spacecraft high-gain antenna may be accurately pointed to Earth for communications, so that onboard experiments may accomplish precise pointing for accurate collection and subsequent interpretation of data, so that the heating and cooling effects of sunlight and shadow ...
The principles of flight dynamics are used to model a vehicle's powered flight during launch from the Earth; a spacecraft's orbital flight; maneuvers to change orbit; translunar and interplanetary flight; launch from and landing on a celestial body, with or without an atmosphere; entry through the atmosphere of the Earth or other celestial body ...
A spacecraft's attitude must typically be stabilized and controlled for a variety of reasons. It is often needed so that the spacecraft high-gain antenna may be accurately pointed to Earth for communications, so that onboard experiments may accomplish precise pointing for accurate collection and subsequent interpretation of data, so that the heating and cooling effects of sunlight and shadow ...
The TRIAD method is the earliest published algorithm for determining spacecraft attitude, which was first introduced by Harold Black in 1964. [1] [2] [3] Given the knowledge of two vectors in the reference and body coordinates of a satellite, the TRIAD algorithm obtains the direction cosine matrix relating to both frames.
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.
Dynamics – maintained the inputs to the mission operation computer for all processors Entry console – provided expert support for entry, approach, and landing Entry support team (ascent and entry) – monitored the winds and weather at the various potential landing sites, prepare trajectory adjustments
Download as PDF; Printable version; In other projects ... Flight dynamics; Spacecraft flight dynamics; Flyby (spaceflight) ... Spacecraft attitude determination and ...
The slew of a spacecraft is its orientation in reference to a plane or fixed position such as Earth, the Sun, another celestial body or other point in space. When moving to assume such an orientation, the spacecraft is slewing. [1] [2] [3] During spaceflight, a craft's attitude must be controlled for reasons depending on the craft's mission ...