SPACECRAFT TURN CONTROL SYSTEM Russian patent published in 2003 - IPC

Abstract RU 2213681 C1

FIELD: automatic control of non-stationary space objects. SUBSTANCE: proposed control system is used for turn of spacecraft to required attitude position. Control system includes control engine unit and setters for setting required angle of turn, permissible angular velocity and minimum acceleration, as well as modulus determination unit, multipliers and computer unit. Provision is also made for selection of minimum signal of spacecraft angular velocity , memory, forming of preset angular velocity and setting of time of turn; system includes also functional amplifier, non-linear gate, etc. Control system optimizes transient processes in speed of response under conditions of high degree of instability of control engine efficiency and parameters of spacecraft due to failure of these engines, change in mass of spacecraft at burning-out of propellant in main cruise engine, etc. EFFECT: reduced consumption of propellant; optimal speed of response of spacecraft. 3 cl, 7 dwg

Similar patents RU2213681C1

Title Year Author Number
SPACECRAFT TURN CONTROL SYSTEM 2002
  • Bonk R.I.
  • Puchkov A.M.
  • Syrov A.S.
RU2213029C1
SPACECRAFT TURN CONTROL SYSTEM 2002
  • Bonk R.I.
  • Puchkov A.M.
  • Syrov A.S.
RU2211787C1
SPACECRAFT TURN CONTROL SYSTEM 2002
  • Bonk R.I.
  • Puchkov A.M.
  • Syrov A.S.
RU2211788C1
SYSTEM FOR CONTROLLING ANGULAR MOTION OF PILOT -FREE AIRCRAFT 2003
  • Bonk R.I.
  • Petushkov B.K.
  • Puchkov A.M.
  • Syrov A.S.
  • Cherepanova V.E.
RU2234117C1
ONBOARD ANGULAR STABILISATION SYSTEM FOR CONTROLLING FLYING AIRCRAFT 2007
  • Syrov Anatolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
  • Cherepanova Valentina Evgen'Evna
  • Kozlov Anatolij Ivanovich
  • Tatsjuk Dmitrij Grigor'Evich
RU2338236C1
CONTROL DEVICE FOR SYSTEM OF COORDINATED CONTROL OF FLIGHT VEHICLE 2003
  • Kravchuk S.V.
  • Puchkov A.M.
  • Syrov A.S.
RU2237269C1
SYSTEM OF IDENTIFICATION OF ARBITRARY TIME OF COMBUSTION OF CRYOGENIC STAGE MASS 2001
  • Syrov A.S.
  • Sokolov V.N.
  • Ezhov V.V.
RU2209157C1
METHOD OF GENERATING CONTROL SIGNAL FOR UNFORCED COOLING OF OVEN ELECTRICAL HEATER AND DEVICE FOR REALISING SAID METHOD 2009
  • Syrov Anatolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
RU2422868C1
METHOD FOR FORMING SIGNAL OF ATTACK ANGLE OF AIRCRAFT AND DEVICE FOR REALIZATION OF SAID METHOD 2003
  • Puchkov A.M.
  • Syrov A.S.
RU2254604C2
METHOD OF IDENTIFICATION OF ARBITRARY TIME OF COMBUSTION OF CRYOGENIC STAGE MASS 2001
  • Syrov A.S.
  • Sokolov V.N.
  • Ezhov V.V.
RU2209158C1

RU 2 213 681 C1

Authors

Bonk R.I.

Puchkov A.M.

Syrov A.S.

Dates

2003-10-10Published

2002-03-01Filed