Dynamics and Simulation of Flexible Rockets

By:   Timothy M. Barrows (Ret. Principal Member Technical Staff Draper Laboratory Cambridge MA USA), Jeb S. Orr (Principal Staff, Flight Systems and CTO, Mclaurin Aerospace, Huntsville, AL, USA)
Imprint:   Academic Press Inc
Country of Publication:   United States
Dimensions:   Height: 229mm,  Width: 151mm, 
Weight:   540g
ISBN:   9780128199947
ISBN 10:   0128199946
Pages:   338
Publication Date:   10 December 2020
Audience:   Professional and scholarly ,  Undergraduate
Format:   Paperback
Publisher's Status:   Active

Dr. Barrows has over 30 years of experience in analysis and simulation of complex mechanical systems for NASA and various agencies of the Department of Defense. His engineering expertise includes aerodynamics, multi-body dynamics, and simulation. A particular expertise is simulation of multibody systems. He has either directly created or supervised the construction of high fidelity simulations of several systems, including the attitude control of a satellite, a generalized robotic manipulator model, the space station mobile transporter, and the flight mechanics of precision guided airdrop systems. Other work has included successful airdrop tests of a gliding autogyro with folding rotor blades, and a concept definition of a large vehicle designed to fly in ground effect. He has served as Section Chief of the Dynamical Systems Group at Draper, in which capacity he served as the engineering task leader of for the Space Station Dynamic Interaction program. During the past ten years, Dr. Barrows has focused on the development of rocket simulations. This has included a wide variety of rockets for both private and government sponsors, culminating in work on NASA’s space launch system. Dr. Jeb Orr has over 16 years of experience in mission-critical software engineering, flight mechanics, model-based design, flight control system architecture, guidance and navigation, structural dynamics, and related disciplines. He has authored or co-authored more than 30 peer-reviewed publications and technical reports and has conducted several invited lectures in the areas of dynamics and control. Dr. Orr has had a key role in various research initiatives supporting NASA and Department of Defense (DoD) emerging technologies. Dr. Orr was a principal designer of the Space Launch System Adaptive Augmenting Control (AAC) algorithm, and developed the FRACTAL software package, now the standard NASA design model for SLS flight control analysis. In 2013 Dr. Orr was awarded the NASA Exceptional Engineering Achievement Medal in recognition of his contributions to the SLS program. Dr. Orr serves as an officer of the SAE/IEEE Aerospace Control and Guidance Systems Committee (ACGSC), and conducts courses in aerospace dynamics and flight control for NASA Marshall Space Flight Center and the NASA Engineering and Safety Center (NESC).