FIELD: space engineering; on-board terminal control facilities of cryogenic stages with non-controllable cruise engines.
SUBSTANCE: parameters of motion of cryogenic stage at moment of cruise engine cutoff are predicted and radius of deviation of radius and radial velocity of cryogenic stage from their preset magnitudes are determined. Signals for correction of pitch angle and rate of pitch are shaped for compensation of said deviation. Pitch angle correction signal is limited at preset level and its excess above this level is determined. When signal is shaped for limitation, addition to correction pitch rate signal is formed. This correction is equal to product of said excess by ratio of functions of sensitivity of radial velocity of cryogenic stage to pitch angle and rate of pitch. Resultant pitch rate correction signal is formed as sum of this signal determined without taking into account pitch angle correction signal limitation and addition. Thus, priority follow-up of velocity error is ensured at limited pitch angle correction.
EFFECT: enhanced accuracy of forming preset orbit due to reduction of disturbance level on angular stabilization loop.
9 dwg, 1 tbl
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RU2223894C1 |
METHOD OF CONTROLLING LONGITUDINAL MOTION OF UPPER-STAGE ROCKET ON DELTA-VELOCITY MANOEUVRE SECTION | 2009 |
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RU2408851C1 |
METHOD OF CORRECTION OF PARAMETERS OF PROGRAM OF CHANGE OF LONGITUDINAL MOTION AT TERMINAL CONTROL OF CRYOGENIC STAGE GUIDANCE TO PRESET ORBIT | 2002 |
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RU2211786C1 |
METHOD OF CONTROL OF BOOSTER UNIT LONGITUDINAL MOTION ON DELTA-VELOCITY MANEUVER PHASE | 2007 |
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Authors
Dates
2005-06-20—Published
2003-06-27—Filed