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ask a number of pilots to fly the given airplane for each phase of flight and then
take an average of all the test results. vfhe Cooper-Harper scale is a systematic
method ofquantifying these test results.lt assigns three levels to describe the flying
qualities of an airplane as follows.4.s
Leve//.   Flying qualities clearly adequate for the mission flight phase.
Leve///.   Flying qualities adequate to accomplish the mission fiight phase when
some increase in pilot workload or degradation in mission effectiveness exists or
both.
/eve////.     Flying qualities such that the mission can be controlled safely, but pilot
workload is excessrve or mission effectiveness is inadequate or both.
592           PERFORMANCE, STABILITY, DYNAMtCS, AND CONTROL
co
a
(/
       Fraquency, racVs
Frequency response: yaw rate
Fig. 630   Frequency response of the general aviation airplane: yaw rate to aileron
inpuL
    Category A fiight phases can be terminated safely, and category B and C fiight
phases can be completed. The fiight phases are divided as follows.
     Category A.    Nonterminal flight phases that require rapid maneuvering, preci-
sion tracking, or precise fiight-path control. Included in the categor}r are air-to-air
combat, ground attack, weapon delivery/launch, aerial recov'er)r, reconnaissance,
in-flight refueling (receiver), terrain following, antisubmarine search, and close-
formation flying.
    Category B.    Nonterminal flight phases that are normally accomplished using
gradual maneuvers and without precision tracking, althoug~'accurate flight-path
control may be required. Included in the category are climb, cruise, loiter, in- flight
refueling (tanker), descent, emergency descent, emergency deceleration, and aerial
delivery.
Termina/ f/ight phases.
  Category C.   Terminal flight phases are normally accomplished using grad-
ual maneuvers and usually re6quire accurate flight-path control. Included in this
category are takeoff, catapult takeoff, approach, wa'veofftgo-around, and landing.
AfRPLANE RESPONSE AND CLOSED-LOOP CONTROL         593
The aircraft are classified as follows.
     Class /.    Small, light airplanes, such as light utility, primary trainer, and light
observation craft.
    Class ///-   Large, heavy, low-to-medium maneuverabilit)t airplanes, such as
heavy transport/cargo/tanker, heavy bomber, and trainer for class III.
     C/ass /V    High-maneuverability airplanes, such as 1ighter/interceptor, attack,
tactical reconnaissance, observation, and trainer for class I'V.
6.4.1   Longitudinal Flying Clua/ities
    Phugoid mode.4,5
Levell = c > 0.04
 Levelll: < > 0
                                                  Levellll = T2 > 55 s
     In the level III, the aircraft is assumed to have an unstable (divergent) phugoid
mode, and T2 denotes the time required for the amplitude to double the init:ial
value.
   The requirements on the natural frequencies of the short-     )d mode4.5 for
category A, B, and C flight phases according to MIL- F~878gtCp6esrihooduld lie within
the linuts as given in Table 6.3.
     Table 6.2   Damping ratios for short-period mode
                                        -7----. _-__-_-___--
                     Cat A and C     Cat A and C     Cat B      Cat B
       <sp.min    Csp,max   Csp,min <rp.max
-_--_ ---~--~-_-_---__-~
Levell    0.35      1.30    0.30   2.0
Levelll    0.25      2.0     0.20   2.0
Levellll   0.15     --    0.15  N
　
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