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68篇 您的检索式:作者名="MEASE K D"
    题名 作者 年代 出处 被引量
1Feasible trajectory generation for at mospheric entry guidance 显示文摘Leavitt J A Mease K D 2007Journal of Guidance Control and Dynamics2007,30,2:1
2Feasible Trajectory Generation for Atmospheric Entry Guidance 显示文摘Leavitt J A Mease K D 2007Journal of Guid- ance Control and Dynamics2007,30,47:1
3Geom-etry and inverse optimality in global attitude stabiliza-tion显示文摘Bharadwaj S Qsipchuk M Mease K D 1998Guid Control Dyna1998,21,6:1
4Re- duced-order entry trajectory planning for acceleration guidance显示文摘MEASE K D CHEN D T TEUFEL P 2002Journal of Guidance Control and Dy- namics2002,25,2:1
5Shuttle entry guidance revisited using nonlinear geometric methods 显示文摘MEASE K D KREMER J P 1994Journal of Guidance Control and Dynamics1994,17,6:1
6Feasible trajectory gen eration for atmospheric entry guidance显示文摘LEAVITT A MEASE K D 2007Journal of Guidance Control and Dynamics2007,30,2:1
7Reduced order entry trajectory planning for acceleration guidance显示文摘Mease K D Chen D T Teufel P 2002Journal of Guidance Control and Dynamics2002,25,2:1
8Reduced-order entry trajectory planning for acceleration guidance 显示文摘Mease K D Chen D T Teufel P 2002Journal of Guidance Control and Dynamics2002,25,2:1
9Reduced-order entry trajectory planning for acceleration guidance显示文摘Mease K D Chen D T Teufel P 2002Journal of Guidance Control and Dynamics2002,25,2:1
10Dichotomic basis approach to solving hypersensitive optimal control problems显示文摘Rao A V and Mease K D 1999Automatica1999,35,:1
11Reduced-order entry trajectory planning for acceleration guidance显示文摘Mease K D Chen D Teufel P and Schonenberger H 2002Journal of Guidance Control and Dynamics2002,25,2:1
12Reduced-order entry trajectory planning for acceleration guidance 显示文摘MEASE K D CHEN D T TEUFEL P 2002Journal of Guidance Control and Dynamics2002,25,2:1
13Reduced-order entry trajectory planning for acceleration guidance 显示文摘Mease K D Chcn D T Schinenberger H 2002Journal of Guidance Control and Dynamics2002,25,2:1
14Minimum Fuel Aeroassisted Coplanar Orbit Transfer Using Lift Modulation显示文摘Mease K D Vinh N X 1985Journal of Guidance Control and Dynamics1985,8,1:1
15Drag-based predictive tracking guidance for Mars preci- sion landing显示文摘TU K Y MUNIR M S MEASE K D Bayard D S 2000Journal of Guidance Control and Dy- namics2000,23,4:1
16Reduced-Order Entry Trajectory Planning for Acceleration Guidance 显示文摘Mease K D Chen D T Teufel P 2002Journal of Guidance Control and Dynamics (S0731-5090)2002,25,2:1
17Ge- ometry and inverse optimality in global attitude sta- bilization 显示文摘BHARADWAJ S QSIPCHUK M MEASE K D 1998Journal of Guidance Control and Dy- namics1998,21,6:1
18Reduced-Order Entry Trajectory Planning for Acceleration Guidance 显示文摘Mease K D Chen D T Teufel P 2002Journal of Guidance Control and Dynamics2002,25,2:1
19Feasible trajectory generation for atmospheric entry guidance显示文摘Leavitt J A Mease K D 2007Journal of Guidance Control and Dynamics2007,30,2:1
20Dichotomic basis approach to solving hyper-sensitive optimal control problems 显示文摘Rao R V Mease K D 1999Automatica1999,35,:1
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