With　the　increase　of　human　activities　in　space,　the　space　robot　has　played　a　more　and　more　important　role.　The　development　of　Space　technology　put　forward　higher　requirements　on　the　performance　of　the　space　robot,　the　dual-arm　space　robot　has　movement　stability　and　load　ability,　will　become　an　important　tool　in　the　future　space　missions.　Space　station　remote　manipulator　system　and　its　end　effector-SPDM　put　into　use,　which　means　that　dual　arm　space　robot　has　been　used　in　the　space.　Dual-arm　system　is　similar　to　the　upper　limbs　of　primate,　which　is　more　advantageous　to　carry　objects,　ensure　the　control　accuracy.　In　the　process　of　space　robot　to　complete　various　missions,　actuators　is　inevitably　impacted　by　target.　Space　robot　itself　is　in　a　state　of　weightlessness　in　space,　which　may　lead　to　large　angle　rotation　is　dangerous　for　the　space　facilities.　For　space　robot　arms　grab　task,　coupling　motion　relations　are　between　arms　and　base,　make　its　control　design　scheme　is　become　more　difficult　than　ground　robot.　In　addition,　the　existences　of　dual-arm　space　robot　with　closed　chain　constraint　and　controller　redundancy　add　the　difficulty　of　control　design.　In　this　paper,　the　impact　effect　analysis　for　a　dual-arm　space　robot　capturing　a　satellite　and　the　coordinated　stabilization　control　problem　for　closed　chain　system　are　discussed.　At　first,　the　dynamic　equations　of　dual-arm　space　robot　and　satellite　are　obtained　by　multi-body　theory.　The　response　of　the　dual-arm　space　robot　impacted　by　the　target　is　analyzed　by　momentum　conservation　law;　the　dynamic　evolution　process　is　derived　at　the　same　time.　Secondly,　the　recurrent　fuzzy　neural　network　control　scheme　is　designed　for　unstable　closed　chain　system　with　uncertain　system　parameter.　In　order　to　overcome　the　effects　caused　by　system　parameter　perturbation　and　external　disturbance,　the　recurrent　fuzzy　neural　network　is　used　to　approximate　the　unknown　part　with　H∞　tracking　characteristic.　Meanwhile,　the　weighted　minimum-norm　theory　is　introduced　to　distribute　torques　guarantee　that　cooperative　operation　between　manipulators.　At　last,　numerical　examples　simulate　the　process　of　collision　and　the　efficiency　of　the　control　scheme　is　verified　by　the　simulation　results.　Copyright　©　2016　by　the　International　Astronautical　Federation.　All　rights　reserved.