An important aspect of rocket flight is
of the rocket.
all use aerodynamic forces to
some measure of flight stability. But these types of toy rockets do not
have any system for flight control.
In order to successfully complete its mission, a
full scale rocket
is designed with systems for both stability and control. The
usually includes sophisticated
sensors and computers to detect the orientation, location, and
speed of the rocket.
To maneuver the rocket in flight, several
can be used. Early rockets,
and some air-to-air missiles, use movable aerodynamic
surfaces like the elevators
on an airplane. Of course, this system only works on
rockets which remain in the atmosphere.
Later rockets designed to exit the atmosphere used small vanes in the
nozzle exhaust to vector
the thrust. Most modern rockets, like the Space Shuttle and the
Saturn V moon rockets, use a system called gimbaled thrust.
In a gimbaled thrust system, the exhaust
of the rocket can be swiveled from side to side. As the nozzle is moved,
the direction of the
is changed relative to the
center of gravity
of the rocket. On the figure at the top we show three case.
The middle rocket shows the "normal" flight configuration in
which the direction of thrust is along the center line
of the rocket and through the center of gravity of the rocket.
On the rocket at the left, the nozzle has been deflected to the left
and the thrust line is now inclined to the rocket center line
at an angle a called the gimbal angle. Since the thrust
no longer passes through the center of gravity, a
is generated about the center of gravity and the nose of the rocket
turns to the left. If the nozzle is gimbaled back along the center line,
the rocket will move to the left.
On the rocket at the right, the nozzle has been deflected to the right
and the nose is moved to the right.
Here's a computer animation of the motion of the rocket as the
nozzle is gimbaled:
a rocket as the nozzle is gimbaled: