By Gunter G. Endres, Graham Edwards
Airline attractiveness consultant КНИГИ ;ВОЕННАЯ ИСТОРИЯ Издательство: HarperCollins PublishersСерия: Jane's popularity GuideАвтор(ы): Gunter Endres, Graham EdwardsЯзык: EnglishГод издания: 2006Количество страниц: 194x2ISBN: 978-0-00-720442-7Формат: pdf (150 dpi) ~1370x1000Размер: 89,3 mb RAPIDили IFOLDER zero
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Extra info for Airline Recognition Guide
For the purposes of this discussion, it is assumed that a system is required to navigate a vehicle which is constrained to move in a single plane. 1. The system contains two accelerometers and a single axis rate gyroscope, all of which are attached rigidly to the body of the vehicle. The vehicle body is represented, in the figure, by the block on which the instruments shown are mounted. 2 Reference frames for two-dimensional navigation vehicle in the plane of motion; they are denoted as the x\> and Zh axes.
9. The diagram displays the main functions to be implemented within a strapdown navigation system; the processing of the rate measurements to generate body attitude, the resolution of the specific force measurements into the inertial reference frame, gravity compensation and the integration of the resulting acceleration estimates to determine velocity and position. 5 Strapdown system mechanisations Attention is focused here on inertial systems which may be used to navigate in the vicinity of the Earth.
7 Illustration of a body reference frame The wander azimuth frame (w-frame) may be used to avoid the singularities in the computation which occur at the poles of the navigation frame. Like the navigation frame, it is locally level but is rotated through the wander angle about the local vertical. 5. 7, is an orthogonal axis set which is aligned with the roll, pitch and yaw axes of the vehicle in which the navigation system is installed. 1 Navigation with respect to a fixed frame Consider the situation where it is required to navigate with respect to a fixed, or non-accelerating, and non-rotating set of axes.