The invention discloses a high-precision
linear motion direct-current driving
system for
spaceflight and a control method of the high-precision
linear motion direct-current driving
system, and relates to the technical field of
spacecraft attitude driving control. The high-precision
linear motion direct current driving control method for
spaceflight comprises the steps of linear
direct current motor response aging judgment,
spacecraft driving load evaluation and
spacecraft driving
signal optimization. According to the method, the driving load influence evaluation requirement is determined through command
signal response timeliness judgment, if the driving load influence evaluation requirement does not exist, the spacecraft attitude adjustment process continues to be monitored, otherwise, the driving
load optimization requirement continues to be determined, and finally if the driving
load optimization requirement exists, the oscillation
signal influence quantification requirement continues to be determined. Otherwise, the oscillation
signal optimization requirement is directly determined after the oscillation signal influences quantification, the spacecraft linear motion
direct current driving stability is improved, and the problem that in the prior art, spacecraft linear motion direct current driving is not stable due to the spacecraft attitude adjustment load requirement difference is solved.