简介：Tobeclosetothepracticalflightprocessandincreasetheprecisionofoptimaltrajectory,asix-degree-offreedom(6-DOF)trajectoryisoptimizedforthereusablelaunchvehicle(RLV)usingtheGausspseudospectralmethod(GPM).DifferentfromthetraditionaltrajectoryoptimizationproblemwhichgenerallyconsiderstheRLVasapointmass,thecouplingbetweentranslationaldynamicsandrotationaldynamicsistakenintoaccount.Anoptimizationproblemisformulatedtominimizeaperformanceindexsubjectto6-DOFequationsofmotion,includingtranslationalandrotationaldynamics.Atwo-stepoptimalstrategyisthenintroducedtoreducethelargecalculationscausedbymultiplevariablesandconvergenceconfinementin6-DOFtrajectoryoptimization.Thesimulationresultsdemonstratethatthe6-DOFtrajectoryoptimalstrategyforRLVisfeasible.