1–34 von 34 Ergebnissen
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    Test Results for Entry Guidance Methods for Space Vehicles

    John Hanson / Robert Jones | AIAA | 2004

    Automated Method to Compute Orbital Reentry Trajectories with Heating Constraints

    Curtis Zimmerman / Greg Dukeman / John Hanson | AIAA | 2003

    Entry Guidance for the X-33 Vehicle

    Ping Lu / John M. Hanson | AIAA | 1998

    Entry trajectory design for the X-33 vehicle

    Lu, Ping / Hanson, John | AIAA | 1997

    An Automated Method to Compute Orbital Re-Entry Trajectories with Heating Constraints

    Zimmerman, Curtis / Dukeman, Greg / Hanson, John | AIAA | 2002

    Improved low-altitude constellation design methods

    HANSON, JOHN M. / LINDEN, ALEXANDER N. | AIAA | 1989

    Optimization of many-burn orbital transfers

    Hanson, John / Dukeman, Gregory | AIAA | 1996

    Designing good partial coverage satellite constellations

    HANSON, JOHN / EVANS, MARIA / TURNER, RONALD | AIAA | 1990

    Ascent, transition, entry, and abort guidance algorithm design for the X-33 vehicle

    Hanson, John / Coughlin, Dan / Dukeman, Gregory et al. | AIAA | 1998

    An alternative entry guidance scheme for the X-33

    Lu, Ping / Hanson, John / Bhargava, Swati | AIAA | 1998

    Flow diagnostics of an arcjet using laser-induced fluorescence

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1992

    Velocity measurements in a hydrogen arcjet using LIF

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1991

    Ascent guidance comparisons

    Hanson, John / Shrader, M. / Cruzen, Craig | AIAA | 1994

    Plume characteristics of an arcjet thruster

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1993

    Entry guidance by trajectory regulation

    Lu, Ping / Shen, Zuojun / Dukeman, Greg et al. | AIAA | 2000

    Laser-induced fluorescence of atomic hydrogen in an arcjet thruster

    LIEBESKIND, JOHN / HANSON, RONALD / CAPPELLI, MARK | AIAA | 1992

    Fuel-optimal, low- and medium-thrust orbit transfers in large numbers of burns

    Chuang, C.-H. / Goodson, Troy / Hanson, John | AIAA | 1994

    Optimal Finite Thrust Orbit Transfers with Large Numbers of Burns

    Troy Goodson / Jason C. H. Chuang / John Hanson | AIAA | 1999

    Optimal non-impulsive thrust orbit transfers with large numbers of burns

    Goodson, Troy / Chuang, C.-H. / Hanson, John | AIAA | 1996

    Shock Tube Measurements of Branched Alkane Ignition Times and OH Concentration Time Histories

    Oehlschlaeger, Matthew / Davidson, David / Herbon, John et al. | AIAA | 2003

    Multiple-Burn Families of Optimal Low- and Medium-Thrust Orbit Transfers

    Jason C. H. Chuang / Troy D. Goodson / John Hanson | AIAA | 1999

    Computation of optimal low- and medium-thrust orbit transfers

    CHUANG, C.-H. / GOODSON, TROY / HANSON, JOHN | AIAA | 1993

    Guidance and dispersion studies of National Launch System ascent trajectories

    HANSON, JOHN / SHRADER, M. / CHANG, HOPEN et al. | AIAA | 1992

    Deterministic reconfigurable control design for the X-33 vehicle

    Wagner, Elaine / Burken, John / Hanson, Curtis et al. | AIAA | 1998

    The second variation and neighboring optimal feedback guidance for multiple burn orbit transfers

    Chuang, , Troy D, C-HGoodson, / Ledsinger, Laura / Hanson, John | AIAA | 1995

    Optimality and guidance for planar multiple-burn orbit transfers

    Chuang, C.-H. / Goodson, Troy D. / Ledsinger, Laura A. et al. | AIAA | 1996

    Transient Plasma Ignition for Delay Reduction in Pulse Detonation Engines

    Cathey, Charles / Wang, Fei / Tang, Tao et al. | AIAA | 2007