Extra-insensitive input shapers for controlling flexible spacecraft
W Singhose, S Derezinski, N Singer - Journal of Guidance, Control, and …, 1996 - arc.aiaa.org
A procedure for designing command profiles for flexible spacecraft is presented. The
command profiles are required to move a spacecraft from rest to rest or to accelerate a
spacecraft to a constant velocity with very little residual vibration. To model the case where
the spacecraft is equipped with on-off reaction jets, the command signals are restricted to
positive or negative constant-amplitude pulses. The technique results in command profiles
that are significantly more robust to modeling errors than profiles developed with similar …
command profiles are required to move a spacecraft from rest to rest or to accelerate a
spacecraft to a constant velocity with very little residual vibration. To model the case where
the spacecraft is equipped with on-off reaction jets, the command signals are restricted to
positive or negative constant-amplitude pulses. The technique results in command profiles
that are significantly more robust to modeling errors than profiles developed with similar …
[PDF][PDF] Extra-Insensitive Input Shapers for Controlling Flexible Spacecraft
S Derezinski, N Singer - JOURNAL OF GUIDANCE, CONTROL, AND …, 1996 - academia.edu
A procedure for designing command profiles for flexible spacecraft is presented. The
cornmand profiles are required to move a spacecraft frum rest to rest or to accelerate a
spacecraft to a constant Velocity with Very little residual vibration. To model the case where
the spacecraft is equipped with on-off reaction jets, the command signals are restricted to
positive or negative constant-amplitude pulses. The technique results in command profiles
that are significantly more robust to nodeling errors than profiles developed with similar …
cornmand profiles are required to move a spacecraft frum rest to rest or to accelerate a
spacecraft to a constant Velocity with Very little residual vibration. To model the case where
the spacecraft is equipped with on-off reaction jets, the command signals are restricted to
positive or negative constant-amplitude pulses. The technique results in command profiles
that are significantly more robust to nodeling errors than profiles developed with similar …
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