导弹制导原理

出版时间:2012-6   出版时间:北京航空航天大学出版社   作者:江加和   页数:312   字数:454000  
封面图片

导弹制导原理
内容概要

The intent of this book is to present
guidance and control principle of tactical missiles. It includes
basicconcepts of guided missile, fundamental concepts of vehicle
dynamics, dynamical equatio and kinematicequatio of vehicle,
longitudinal state equation and trafer functio, lateral state
equation and traferfunctio, fundamental principle of missile
guidance and control system, guidance laws, autopilot
design,command guidance systems, homing guidance systems, and
guidance and control system hardware-in-the-loopsimulation. This
book is suitable for international postgraduate and advanced
undergraduates majoring in navigation,guidance and control, and
also suitable for engineering and technical peonnel engaged in the
design anddevelopment of guided missiles.
书籍目录

CHAPTER 1 Introduction to Missile Guidance
CHAPTER 2 Basic Knowledge of Flight Dynamics
CHAPTER 3 Equatio of Motion for Vehicle
CHAPTER 4 Longitudinal Motion
CHAPTER 5 Lateral Motion
CHAPTER 6 Flight Control of Missile
CHAPTER 7 Guidance Laws
CHAPTER 8 Autopilot Design
CHAPTER 9 Command Guidance Systems
CHAPTER 10 Homing Guidance Systems
CHAPTER 11 Hardware-in-the-loop Simulation of Guidance and Control
System
章节摘录

版权页:
插图:
When
a
vehicle
flies
in
the
air,it
undergoes
resistance
which
the
air
exerts.In
order
to
overcome
the
resistance,it
is
necessary
to
consume
engine
power.Not
only
the
vehicle
wings
produce
resistance,but
also
any
other
part
exposing
to
the
air
yields
resistance.So
the
wing
resistance
can
not
represent
the
total
resistance.
As
for
a
low
speed
vehicle,there
are
the
friction
resistance,the
pressure
deference
resistance,and
the
induced
resistance.For
a
supersonic
vehicle,the
shock
wave
results
in
the
wave
resistance.Anyway,the
coefficient
of
drag
consists
of
two
terms
as
follows:
Co=CoO+Coi
(2.4-13)
where
CD0=zero
lift
drag
coefficient,
CDi=lift
induced
drag
coefficient.
In
the
case
of
a
small
angle
of
attack,the
drag
coefficient
is
represented
as
CD=-CDo(Ma)+K(Ma)C2L
(2.4-14)
Moreover,the
drag
coefficient
depends
on
Mach
number.Figure
2.4-5
shows
the
CDo
versus
Mach
number
Ma
curve
in
the
case
of
α=0.
Figure
2.4-6
shows
the
CL
versus
CD
curve,called
lift-drag
polar
curve.It
indicates
that
a
vehicle
gets
lift
at
the
cost
of
producing
resistance.
编辑推荐

《导弹制导原理》由北京航空航天大学出版社出版。
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武器工业
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