Pee Wee: Small and bold as a merlin, the tiniest hawk of them all. Wise-cracking navigator who flies the amazing rocket ship Phoenix and laughs at danger. Agatha June: Flies like a dove, strikes like a falcon.
#1G FORCE CRACK#
A crack marksman with the eye of an eagle and nerves of steel. Strong, vigilant, fearless as a hawk, guarding the four young agents under his command. Narrator: Five teenage champions! G-Force: Guardians of Space! Fighting for good over evil, fighting to defend planet Earth from deadly enemies from space. In the show, five brave teenagers - Ace Goodheart, Dirk Daring, Agatha June, Pee Wee and Hoot Owl battle the aliens Galactor and Computor for the fate of the planet Earth. With G-Force, Sandy Frank Entertainment collaborated with Turner Broadcasting to create a newer, more faithful translation of Science Ninja Team Gatchaman for a new audience, and such a translation was made possible with the relaxed television standards of the 1980s, a luxury that the more Star Wars-themed Battle of the Planets did not enjoy.
#1G FORCE SERIES#
All rights reserved.G-Force: Guardians of Space ( 1986) is the second American animated television adaptation of the Japanese anime series Science Ninja Team Gatchaman ( 1972), following Sandy Frank Entertainment's initial 1978 effort Battle of the Planets and preceding ADV Films' 2005 attempt, known merely as Gatchaman. This is commonly called "stick force per g."Ĭopyright © The Boeing Company. This description of maneuvering flight points out that maneuvering stability for a given configuration manifests itself to the flight crew as the column force required to maintain a certain level of g. If the column force is released, the pitching moment due to the elevator or stabilizer goes to zero, and the moments due to pitch rate and angle of attack drive the pitch rate to zero, and the airplane returns to 1 g flight. Since the pitching moments are now balanced, the pilot must hold the column force. At this point, if the force is maintained, and there is enough thrust to maintain airspeed, the airplane stabilizes at a new angle of attack, with corresponding changes in lift and g. The column force generates a pitching moment through the elevators, or stabilizer in some airplanes, that is eventually balanced by the damping moment created by the horizontal tail and the moment due to the change in angle of attack. For most airplanes, static stability attempts to maintain the airplane in 1 g flight at the trimmed angle of attack. It is a measure of the longitudinal stability tendencies of the airplane in other than 1 g flight, and it accounts for the effects of pitch rate aerodynamic damping during maneuvering, as in the recovery from a pitch upset.Ī column force is required to maneuver longitudinally. Maneuvering stability is related to static longitudinal stability. This plot graphically demonstrates that maneuvering at high-altitude requires less column force than it does at low altitude. While the plot shows that the airplane is still more stable at a forward CG than an aft CG, it also shows that altitude greatly affects the force required to pull the same 2 g at any CG location. For example, to perform a level turn at 60 degrees of bank requires 2 g in any airplane. This has significant consequences for steep turning maneuvers. In other words, at any altitude, the stick force per g is higher when the CG is forward than when the CG is further aft. The maneuvering stability, or stick force per g, is higher at a forward CG, regardless of altitude. The plot makes it obvious that CG location and its effect on positive longitudinal static stability influence maneuvering stability. Called friction and breakout, this situation results from the need to overcome control column static friction and the feel system centering spring.
The lower-left corner of the graph shows that a certain amount of force must be applied before the airplane starts to move from 1 g flight. The lower the slope, the less the maneuvering stability. The left axis displays elevator column force values that increase in the up direction, while the bottom axis displays normal acceleration ( g) values that increase in the right direction. It does not represent the data for any specific airplane, but instead reflects the typical maneuvering stability characteristics of a conventional, unaugmented airplane. Figure 2 depicts a plot of control column force as it relates to normal acceleration for a stable airplane.
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