My question is about the variables that are used in
the autopilot system. As far as I can understand the target heading is
calculated by the angle between the aircraft and the waypoint with the proper
heading and the rate of change of angle times the distance between the
coordinates which ar
Do you use any program to calculate the
coefficients of rolling, pitching,yawing moments and the drag, lift and
sideforce coefficients. The conf file of Cessna seemed so complete containing
all of those coefficients. I am trying to change the aircraft
properties for different types of airpla
I have downloaded a matlab-simulink program that
uses flightgear interface. For a flight dynamics model it requires external fdm
so I command from that program and visualise in flight gear. My question
is how can I change the flight dynamics model to the external type. I
read that batch fil
my operating system is windows milenium and I tried
to change my aircraft via entering
flight\FlightGear\runfgfs.bat ''--aircraft=4a-yasim''
into the start\run directory but the simulation
didn't start.
"You can also pass command line options from Sec.
4
to the batch file (if running it fo
my operating system is windows milenium and I tried to change my aircraft
via entering
flight\FlightGear\runfgfs.bat ''--aircraft=4a-yasim''
into the start\run directory but the simulation didn't start.
"You can also pass command line options from Sec. 4 to the batch file (if
running it form a Co
Firstly I want to thank you for your help in my
understanding of the aerodynamic structure of the aircrafts.
I have two questions about the aerodynamics
model
firstly I have a program that calculates lift and
drag versus attack angle coefficients for a given parameterised airfoil and
is it
I am trying to change some code in the flight
gear modules and I have a great problem compiling it with mcrsoft visual
c++. How can I compile the new code. I heard that makefiles can be
used for compilation. Do they work in windows millenium. If you
can direct me with some information I wo
I have a couple of questions that I am not sure of about the
calculation of target heading. is the nav heading the heading from the north
or the difference between our aircrafts and the navigation points heading
angles and is the nav radial the angle between the aircraft to the waypo
I have a couple of questions that I am not sure of about the
calculation of target heading. is the nav heading the heading from the north
or the difference between our aircrafts and the navigation points heading
angles and is the nav radial the angle between the aircraft to the waypoint
wi
Thank you for your reply and I began to understood the concepts of
the heading hold system in nav mode but some of the autopilot system's
properties are not so solid in my mind so I want to briefly summarase my
understanding of the autopilot systems lateral navigation mode if there are
If the heading mode is FG_HEADINGWAY_POINT does autopilot block use
a similar procedure like in VOR or ILS navigation by using a rolling motion
to intersect waypoint in a pre-determined heading or does it use the angle
difference between its current heading and the heading calculated by t
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