To present the kinematic modeling useful in all flight dynamic derivations and analyses.

    To offer a rigorous vector analysis of rotational kinematics.

    To derive the basic identities of coordinate transformations in a manner that can be easily utilized for both translational and rotational equations of motion in subsequent chapters.

    To introduce several alternative kinematic representations (Euler angles, Euler axis/principal angle, rotation matrix, quaternion, Rodrigues and modified Rodrigues parameters) and their evolution in time.


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    Title :

    Attitude and Kinematics of Coordinate Frames


    Additional title:

    Modeling,Simulation in Science(Birkhäuser)



    Publication date :

    2007-01-01


    Size :

    36 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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