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Books > Professional & Technical > Transport technology > Aerospace & aviation technology
This book presents fundamental theories, design and testing
methodologies, and engineering applications concerning spacecraft
thermal control systems, helping readers gain a comprehensive
understanding of spacecraft thermal control systems and
technologies. With abundant design methods, advanced technologies
and typical applications to help them grasp the basic concepts and
principles of engineering applications, it is mainly intended for
engineering and technical staff engaged in spacecraft thermal
control areas. The book discusses the thermal environments commonly
used for space flight missions, rules and regulations for system
design, thermal analysis and simulation, and thermal testing
methods, as well as the design and validation of the thermal
control systems for Chinese spacecraft, such as the Shenzhou
spacecraft and Chang'e Lunar Lander and Rover. It also introduces
them to communication and remote sensing satellites and presents
advanced thermal control technologies developed in recent years,
including heat transfer, heat insulation, heating, refrigeration
and thermal sensor technologies. Addressing the design and
validation of thermal control systems for various types of Chinese
spacecraft, the book offers a valuable theoretical and practical
reference guide for researchers and engineers alike.
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Pilots
(Hardcover)
K Terry Cf Bobby K Terry Cfii, Bobby K. Terry Sr. CFII
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R919
Discovery Miles 9 190
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Ships in 12 - 19 working days
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This book introduces the concept of unsteady aerodynamics and its
underlying principles. The author provides the readers with a
comprehensive review of the fundamental physics of free and forced
unsteadiness, the terminology and basic equations of aerodynamics
ranging from incompressible flow to hypersonics. The book also
covers modern topics related to the developments made in recent
years, especially in relation to wing flapping for propulsion. The
book is written for graduate and senior year undergraduate students
in aerodynamics and also serves as a reference for experienced
researchers. Each chapter includes ample examples, questions,
problems and relevant references. This 3rd edition includes a new
chapter about unsteady applications related to the thrust
optimization, aerodynamic stability and trim because there has been
much progress in unsteady applications of the flapping wing
technology. In addition, further material is presented in Appendix
for evaluating the stability derivatives so that no derivation of
equations is left incomplete but not overdone in the text.
This book explores key techniques and methods in electromagnetic
compatibility management, analysis, design, improvement and test
verification for spacecraft. The first part introduces the general
EMC technology of spacecraft, the electromagnetic interference
control method and management of electromagnetic compatibility. The
second part discusses the EMC prediction analysis technique and its
application in spacecraft, while the third presents the EMC design
of spacecraft modules and typical equipment. The final two parts
address spacecraft magnetic design testing technologies and
spacecraft testing technologies. The book also covers the program
control test process, the special power control unit (PCU),
electric propulsion, PIM test and multipaction testing for
spacecraft, making it a valuable resource for researchers and
engineers alike.
At the age of 17, Samuel L. Broadnax--enamored with
flying--enlisted and trained as a pilot at the Tuskegee Army Air
Base. Although he left the Air Corps at the end of the Second World
War, his experiences inspired him to talk with other pilots and
black pioneers of aviation. Blue Skies, Black Wings recounts the
history of African Americans in the skies from the very beginnings
of manned flight. From Charles Wesley Peters, who flew his own
plane in 1911, and Eugene Bullard, a black American ace with the
French in World War I, to the 1945 Freeman Field mutiny against
segregationist policies in the Air Corps, Broadnax paints a vivid
picture of the people who fought oppression to make the skies their
own.
The book highlights three types of technologies being developed for
autonomous solution of navigation problems. These technologies are
based on the polarization structure, ultra-broadband and the
fluctuation characteristics (slow and fast) of the radiolocation
signals. The book presents the problems of intrinsic thermal radio
emission polarization and change in radio waves polarization when
they are reflected from objects with non-linear properties. The
purpose of this book is to develop the foundations for creating
autonomous radionavigation systems to provide aviation with
navigation systems that will substantially increase its
capabilities, specifically acting where satellite technologies do
not work. The book is intended for specialists involved in the
development and operation of aviation-technical complexes, as well
as for specialists of national aviation regulators and ICAO experts
dealing with the problems of improving flight safety.
This book focuses on gyro-free inertial navigation technology,
which is used to measure not only linear motion parameters but also
angular rates. Since no gyroscopes are used, the key technologies,
such as initial alignment, attitude resolution, and error
calibration, are very different than those used in traditional
methods. Discussing each key technology in gyro-free inertial
navigation system (GFINS) manufacture in a separate chapter, the
book features easy-to-understand, detailed illustrations, to allow
all those involved in inertial navigation to gain a better grasp of
GFINS manufacture, including accelerometer setting principles;
initial alignment; quaternion-based, attitude resolution
algorithms; and accelerometer de-noise methods.
Recent advances in scientific computing have caused the field of
aerodynamics to change at a rapid pace, simplifying the design
cycle of aerospace vehicles enormously - this book takes the
readers from core concepts of aerodynamics to recent research,
using studies and real-life scenarios to explain problems and their
solutions. This book presents in detail the important concepts in
computational aerodynamics and aeroacoustics taking readers from
the fundamentals of fluid flow and aerodynamics to a more in-depth
analysis of acoustic waves, aeroacoustics, computational modelling
and processing. This book will be of use to students in multiple
branches of engineering, physics and applied mathematics.
Additionally, the book can also be used as a text in professional
development courses for industry engineers and as a self-help
reference for active researchers in both academia and the industry.
This book provides novel concepts and techniques for air traffic
management (ATM) and communications, navigation, and surveillance
(CNS) systems. The book consists of selected papers from the 6th
ENRI International Workshop on ATM/CNS (EIWAC2019) held in Tokyo in
October 2019, the theme of which was "Exploring Ideas for World
Aviation Challenges". Included are key topics to realize safer and
more efficient skies in the future, linked to the integrated
conference theme consisting of long-term visions based on
presentations from various fields. The book is dedicated not only
to researchers, academicians, and university students, but also to
engineers in the industry, air navigation service providers
(ANSPs), and regulators of aviation.
This book systematically presents the concept, history,
implementation, theory system and basic methods of pulsar and space
flight, illustrating the characteristics of pulsars. It also
describes the classification of spacecraft navigation systems and
the autonomous navigation technologies, as well as X-ray
pulsar-based navigation systems (XPNAV) and discusses future
navigation satellite systems in detail.
This book presents iterative learning control (ILC) to address
practical issues of flexible structures. It is divided into four
parts: Part I provides a general introduction to ILC and flexible
structures, while Part II proposes various types of ILC for simple
flexible structures to address issues such as vibration, input
saturation, input dead-zone, input backlash, external disturbances,
and trajectory tracking. It also includes simple partial
differential equations to deal with the common problems of flexible
structures. Part III discusses the design of ILC for flexible micro
aerial vehicles and two-link manipulators, and lastly, Part IV
offers a summary of the topics covered. Unlike most of the
literature on ILC, which focuses on ordinary differential equation
systems, this book explores distributed parameter systems, which
are comparatively less stabilized through ILC.Including a
comprehensive introduction to ILC of flexible structures, it also
examines novel approaches used in ILC to address input constraints
and disturbance rejection. This book is intended for researchers,
graduate students and engineers in various fields, such as flexible
structures, external disturbances, nonlinear inputs and tracking
control.
This book describes the development and design of a unique combined
data and power management infrastructure for small satellites. This
new edition became necessary because in the frame of the system's
impressive evolution from an academic prototype to one of today's
most advanced core avionics, many elements were upgraded to their
next technology generation and diverse new components complement
the upgraded design. All elements are presented in updated
respectively new chapters. This modular infrastructure was selected
by the Swiss start-up ClearSpace SA for ESA's first mission
ClearSpace-1 to remove space debris. Furthermore it is the baseline
for the Thai national satellite development program and is used by
an increasing number of universities worldwide for research
studies.
This book introduces readers to the fundamentals of estimation and
dynamical system theory, and their applications in the field of
multi-source information fused autonomous navigation for
spacecraft. The content is divided into two parts: theory and
application. The theory part (Part I) covers the mathematical
background of navigation algorithm design, including parameter and
state estimate methods, linear fusion, centralized and distributed
fusion, observability analysis, Monte Carlo technology, and linear
covariance analysis. In turn, the application part (Part II)
focuses on autonomous navigation algorithm design for different
phases of deep space missions, which involves multiple sensors,
such as inertial measurement units, optical image sensors, and
pulsar detectors. By concentrating on the relationships between
estimation theory and autonomous navigation systems for spacecraft,
the book bridges the gap between theory and practice. A wealth of
helpful formulas and various types of estimators are also included
to help readers grasp basic estimation concepts and offer them a
ready-reference guide.    Â
This book offers a comprehensive overview of recently developed
space multi-tethers, such as maneuverable space tethered nets and
space tethered formation. For each application, it provides
detailed derivatives to describe and analyze the mathematical model
of the system, and then discusses the design and proof of different
control schemes for various problems. The dynamics modeling
presented is based on Newton and Lagrangian mechanics, and the book
also introduces Hamilton mechanics and Poincare surface of section
for dynamics analysis, and employs both centralized and distributed
controllers to derive the formation question of the multi-tethered
system. In addition to the equations and text, it includes 3D
design drawings, schematic diagrams, control scheme blocks and
tables to make it easy to understand. This book is intended for
researchers and graduate students in the fields of astronautics,
control science, and engineering.
This book presents the results of a European-Chinese collaborative
research project, Manipulation of Reynolds Stress for Separation
Control and Drag Reduction (MARS), including an analysis and
discussion of the effects of a number of active flow control
devices on the discrete dynamic components of the turbulent shear
layers and Reynolds stress. From an application point of view, it
provides a positive and necessary step to control individual
structures that are larger in scale and lower in frequency compared
to the richness of the temporal and spatial scales in turbulent
separated flows.
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