TY  - BOOK
AU  - Zipfel,Peter H.
TI  - Modeling and simulation of aerospace vehicle dynamics
T2  - Aiaa education series
SN  - 1563478757
U1  - 629.13230151 
PY  - 2007///
CY  - [S.l.]
PB  - AIAA (American Institute of Aeronautics & Ast
KW  - Aerodynamics - Mathematics
KW  - Airplanes - Mathematical models
KW  - Space vehicles - Dynamics - Mathematical models
KW  - Technology & Industrial Arts
KW  - Aeronautics & Astronautics
KW  - Technology & Engineering / Aeronautics & Astronautics
KW  - Astrophysics & Space Science
KW  - Aerospace & aviation technology
KW  - Astrophysics
KW  - Mathematics & science
KW  - Technology & Engineering
KW  - Science/Mathematics
KW  - Aerodynamics
KW  - Airplanes
KW  - Dynamics
KW  - Mathematical models
KW  - Mathematics
KW  - Space vehicles
KW  - Mechanical engineering
N1  - This book unifies all aspects of flight dynamics for the efficient development of aerospace vehicle simulations. Now in its second edition, its purpose is still to provide the reader with a complete set of tools to build, program, and execute simulations. Unlike other books, it uses tensors for modeling flight dynamics in a form invariant under coordinate transformations. For implementation, the tensors are converted into matrices, resulting in compact computer code. The reader can pick FORTRAN templates of missiles, aircraft, or hypersonic vehicles from the complimentary "CADAC" CD-ROM to jump-start a particular application, and plot the results of CADAC Studio. It is the only textbook that combines the theory of modeling with hands-on examples of three-, five-, and six-DoF simulations. This new and enlarged edition also serves as anchor for a self-tutoring, three-part course of aerospace simulations in C++, available from AIAA. Amply illustrated with 318 figures and 44 examples, the text can be used for advanced undergraduate and graduate instruction or for self-study. Seventy eight problems and nine projects amplify the topics and develop the material further. Qualified instructors can obtain a complimentary solution manual from AIAA. This second edition contains two new appendices. The original Appendix C, which reviewed state-of-the-art FORTRAN simulations, has been replaced by the description of three self-study CD-ROMs of aerospace simulations in C++. These CDs broaden the applications of this book by spanning from simple three degrees of freedom cruise missiles to high fidelity missiles, aircraft, and hypersonic vehicles. The new Appendix D lays the theoretical foundation of tensor flight dynamics. It contains the proofs of the rotational time derivative and the Euler transformation
ER  -