Stability And Control Of Conventional And Unconventional Aerospace Vehicle Configurations
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Author | : Bernd Chudoba |
Publisher | : Springer |
Total Pages | : 392 |
Release | : 2019-07-23 |
Genre | : Technology & Engineering |
ISBN | : 3030168565 |
This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?
Author | : Bernd Chudoba |
Publisher | : Books on Demand |
Total Pages | : 294 |
Release | : 2001 |
Genre | : Aerodynamics |
ISBN | : 9783831129829 |
Author | : Bernd Chudoba |
Publisher | : |
Total Pages | : |
Release | : 2001 |
Genre | : |
ISBN | : |
Author | : W. J. Duncan |
Publisher | : Cambridge University Press |
Total Pages | : 409 |
Release | : 2016-02-04 |
Genre | : Technology & Engineering |
ISBN | : 1316509745 |
First published in 1959, this book provides a detailed discussion regarding control and stability in aircraft, encompassing the broader subject of aircraft dynamics. Information on newer discoveries related to the effects of compressibility of air and the deformation of aircraft structures is included.
Author | : Bernard Etkin |
Publisher | : John Wiley & Sons |
Total Pages | : 403 |
Release | : 1995-10-31 |
Genre | : Technology & Engineering |
ISBN | : 0471034185 |
Designed to prepare students to become aeronautical engineers who can face new and challenging situations. Retaining the same philosophy as the two preceding editions, this update emphasizes basic principles rooted in the physics of flight, essential analytical techniques along with typical stability and control realities. This edition features a full set of exercises and a complete Solution's Manual. In keeping with current industry practice, flight equations are presented in dimensional state-vector form. The chapter on closed-loop control has been greatly expanded with details on automatic flight control systems. Uses a real jet transport (the Boeing 747) for many numerical and worked-out examples.
Author | : Robert C. Nelson |
Publisher | : McGraw-Hill Companies |
Total Pages | : 304 |
Release | : 1989 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : Brian L. Stevens |
Publisher | : John Wiley & Sons |
Total Pages | : 768 |
Release | : 2015-10-02 |
Genre | : Technology & Engineering |
ISBN | : 1118870972 |
Get a complete understanding of aircraft control and simulation Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is a comprehensive guide to aircraft control and simulation. This updated text covers flight control systems, flight dynamics, aircraft modeling, and flight simulation from both classical design and modern perspectives, as well as two new chapters on the modeling, simulation, and adaptive control of unmanned aerial vehicles. With detailed examples, including relevant MATLAB calculations and FORTRAN codes, this approachable yet detailed reference also provides access to supplementary materials, including chapter problems and an instructor's solution manual. Aircraft control, as a subject area, combines an understanding of aerodynamics with knowledge of the physical systems of an aircraft. The ability to analyze the performance of an aircraft both in the real world and in computer-simulated flight is essential to maintaining proper control and function of the aircraft. Keeping up with the skills necessary to perform this analysis is critical for you to thrive in the aircraft control field. Explore a steadily progressing list of topics, including equations of motion and aerodynamics, classical controls, and more advanced control methods Consider detailed control design examples using computer numerical tools and simulation examples Understand control design methods as they are applied to aircraft nonlinear math models Access updated content about unmanned aircraft (UAVs) Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is an essential reference for engineers and designers involved in the development of aircraft and aerospace systems and computer-based flight simulations, as well as upper-level undergraduate and graduate students studying mechanical and aerospace engineering.
Author | : Joseph R. Chambers |
Publisher | : |
Total Pages | : 50 |
Release | : 1966 |
Genre | : Airplanes |
ISBN | : |
Author | : Gary John Coleman (Jr) |
Publisher | : |
Total Pages | : 283 |
Release | : 2007 |
Genre | : |
ISBN | : 9781109815306 |
During the conceptual design (CD) phase, various solution concepts must, and should, be explored to select the best flight vehicle size and configuration in order to meet the mission requirements. As the aerospace industry advances novel aerospace flight vehicle configurations promising larger operational performance and overall efficiency, demanding integrated flight vehicles like the flying wing configuration (FWC) or blending wing body (BWB) are under investigation. Some of these novel configurations rely on novel control effectors (CE) and complex flight control systems in order to obtain the desired performance objectives. Clearly, stability and control plays an important roll in the design of advanced flight vehicles.
Author | : Duane T. McRuer |
Publisher | : |
Total Pages | : 116 |
Release | : 1962 |
Genre | : Aerodynamics |
ISBN | : |
Conventional aeronautical stability and control usage is extended into the aerospace flight regime with particular reference to the definition of operating points and coordinate systems. Implied and studied in this extension are the basic particle-dynamic equations of motion, magnitudes of possible external forces, and the flight regimes of fundamental interest. Simplified solutions of the particle-dynamic equations of motion are obtained, and certain low-frequency modes common to both particle and rigid-body motion are explored.