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Finally, we present the actual flight attitude data of IKAROS and the change of its trajectory.
The key technique of a kinetic energy rod (KER) warhead is to control the flight attitude of rods.
It is shown that such a reconfigurable flight control design is valid, through numerical simulations of flight attitude control task.
For dynamic in situ flying height and flight attitude measurements, a prototype of a thermal test head has been developed.
Leaders use hand signals, head nods, aircraft movements, or radio calls to alert their wingmen of changes in flight attitude, formation positions, split-ups, rejoins, and radio frequencies.
Since Small Unmanned Helicopter flight attitude control process has strong time- varying characteristics, and there are random disturbances, the conventional control methods with unchanged parameters are often unworkable.
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The flight attitudes and control inputs of aircraft during touchdown can significantly influence the landing impacts.
The external heat flux of orbiting solar array in these orbits is proposed according to the flight attitudes.
The resulting flight attitudes and control inputs are presented for different control strategies and compared to the results of landing simulations with a conventional landing gear.
Further improvements were introduced throughout the Merlin series, with Bendix-manufactured pressure carburettors, which were designed to allow fuel to flow during all flight attitudes, introduced in 1942.
Pilots obtain additional certificates as they progress up the skill ladder and are tested completely for emergencies, including unusual flight attitudes such as partial and full stalls.
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