1.2.2.1 At a given engine output and rudder angle
δ, the ship may take up a certain steady motion. In general, this
will be a turning motion with constant yaw rate ψ, speed V and
drift angle β (bow-in). The radius of the turn is then defined
by the following relationship, expressed in consistent units:
1.2.2.2 This particular ship-rudder angle configuration
is said to be "dynamically stable in a turn of radius R". Thus, a
straight course may be viewed as part of a very wide circle with an
infinite radius, corresponding to zero yaw rate.
1.2.2.3 Most ships, perhaps, are "dynamically
stable on a straight course" (usually referred to as simply "dynamically
stable") with the rudder in a neutral position close to midship. In
the case of a single screw ship with a right-handed propeller, this
neutral helm is typically of the order δo = -1°
(i.e., 1° to starboard). Other ships which are dynamically unstable,
however, can only maintain a straight course by repeated use of rudder
control. While some instability is fully acceptable, large instabilities
should be avoided by suitable design of ship proportions and stern
shape.
1.2.2.4 The motion of the ship is governed mainly
by the propeller thrust and the hydrodynamic and mass forces acting
on the hull. During a manoeuvre, the side force due to the rudder
is often small compared to the other lateral forces. However, the
introduced controlling moment is mostly sufficient to balance or overcome
the resultant moment of these other forces. In a steady turn there
is complete balance between all the forces and moments acting on the
hull. Some of these forces seeming to "stabilize" and others to "destabilize"
the motion. Thus the damping moment due to yaw, which always resists
the turning, is stabilizing and the moment associated with the side
force due to sway is destabilizing. Any small disturbance of the equilibrium
attitude in the steady turn causes a change of the force and moment
balance. If the ship is dynamically stable in the turn (or on a straight
course) the net effect of this change will strive to restore the original
turning (or straight) motion.
1.2.2.5 The general analytical criterion for dynamic
stability may be formulated and evaluated with the appropriate coefficients
of the mathematical model that describes the ship’s motion.
The criterion for dynamic stability on a straight course includes
only four "linear stability derivatives" which together with the centre-of-gravity
position, may be used to express the "dynamic stability lever". This
lever denotes the longitudinal distance from the centre-of-pressure
of the side force due to pure sway (or sideslip) to the position of
the resultant side force due to pure turning, including the mass force,
for small deviations from the straight-line motion. If this distance
is positive (in the direction of positive x, i.e. towards the bow)
the ship is stable. Obviously "captive tests" with a ship model in
oblique towing and under the rotating arm will furnish results of
immediate interest.
1.2.2.6 It is understood that a change of trim
will have a marked effect mainly on the location of the centre-of-pressure
of the side force resulting from sway. This is easily seen that a
ship with a stern trim, a common situation in ballast trial condition,
is likely to be much more stable than it would be on an even draught.
1.2.2.7 Figure 1 gives an example of the equilibrium yaw-rate/rudder
angle relation for a ship which is inherently dynamically unstable on a straight
course. The yaw rate is shown in the non-dimensional form for turn path curvature
discussed above. This diagram is often referred to as "the spiral loop curve" because
it may be obtained from spiral tests with a ship or model. The dotted part of the
curve can only be obtained from some kind of reverse spiral test. Wherever the slope
is positive, which is indicated by a tangent sloping down to the right in the
diagram, the equilibrium balance is unstable. A ship which is unstable on a straight
course will be stable in a turn despite the rudder being fixed in the midship or
neutral position. The curvature of this stable turn is called "the loop height" and
may be obtained from the pullout manoeuvre. Loop height, width and slope at the
origin may all be regarded as a measure of the instability.
1.2.2.8 If motion is not in an equilibrium turn,
which is the general case of :notion, there are not only unbalanced
damping forces but also hydrodynamic forces associated with the added
inertia in the flow of water around the hull. Therefore, if the rudder
is left in a position the ship will search for a new stable equilibrium.
If the rudder is shifted (put over "to the other side") the direction
of the ship on the equilibrium turning curve is reversed and the original
yaw tendency will be checked. By use of early counter-rudder it is
fully possible to control the ship on a straight course with helm
angles and yaw rates well within the loop.
1.2.2.9 The course-keeping ability or "directional
stability" obviously depends on the performance of the closed loop
system including not only the ship and rudder but also the course
error sensor and control system. Therefore, the acceptable amount
of inherent dynamic instability decreases as ship speed increases,
covering more ship lengths in a given period of time. This results
because a human helmsman will face a certain limit of conceptual capacity
and response time. This fact is reflected in the IMO Standards for
ship manoeuvrability where the criterion for the acceptable first
overshoot in a zig-zag test includes a dependence on the ratio L/V,
a factor characterizing the ship "time constant" and the time history
of the process.
1.2.2.10 In terms of control engineering, the
acceptable inherent instability may be expressed by the "phase margin"
available in the open loop. If the rudder is oscillated with a given
amplitude, ship heading also oscillates at the same frequency with
a certain amplitude. Due to the inertia and damping in the ship dynamics
and time delays in the steering engine, this amplitude will be smaller
with increasing frequency, meaning the open loop response will lag
further and further behind the rudder input. At some certain frequency,
the "unit gain" frequency, the response to the counter-rudder is still
large enough to check the heading swing before the oscillation diverges
(i.e., the phase lag of the response must then be less than 180°).
If a manual helmsman takes over the heading control, closing the steering
process loop, a further steering lag could result but, in fact, he
will be able to anticipate the swing of the ship and thus introduce
a certain "phase advance". Various studies suggest that this phase
advance may be of the order of 10° to 20°. At present there
is no straightforward method available for evaluating the phase margin
from routine trial manoeuvres.
1.2.2.11 Obviously the course-keeping ability
will depend not only upon the counter-rudder timing but also on how
effectively the rudder can produce a yaw checking moment large enough
to prevent excessive heading error amplitudes. The magnitude of the
overshoot angle alone is a poor measure for separating the opposing
effects of instability and rudder effectiveness, additional characteristics
should therefore be observed. So, for instance, "time to reach second
execute", which is a measure of "initial turning ability", is shortened
by both large instability and high rudder effectiveness.
1.2.2.12 It follows from the above that a large dynamic
instability will favour a high "turning ability" whereas the large yaw damping, which
contributes to a stable ship, will normally be accompanied by a larger turning
radius. This is noted by the thin full-drawn curve for a stable ship included in
figure 1.
1.2.2.13 Hard-over turning ability is mainly an
asset when manoeuvring at slow speed in confined waters. However,
a small advance and tactical diameter will be of value in case emergency
collision avoidance manoeuvres at normal service speeds are required.
1.2.2.14 The "crash-stop" or "crash-astern" manoeuvre
is mainly a test of engine functioning and propeller reversal. The
stopping distance is essentially a function of the ratio of astern
power to ship displacement. A test for the stopping distance from
full speed has been included in the Standards in order to allow a
comparison with hard-over turning results in terms of initial speed
drop and lateral deviations.