|
|
|
|
| LEADER |
00000cam a2200000 i 4500 |
| 001 |
41fd20ce-508c-409c-a69f-1c7eb43bb931 |
| 005 |
20240705000000.0 |
| 008 |
130328t20132013caua b 101 0 eng d |
| 020 |
|
|
|a 0877035911
|
| 020 |
|
|
|a 9780877035916
|
| 035 |
|
|
|a (OCoLC)833301857
|
| 040 |
|
|
|a YDXCP
|b eng
|e rda
|c YDXCP
|d AAA
|d FDA
|
| 050 |
|
4 |
|a TL787.A6
|b A2 v. 146
|
| 111 |
2 |
|
|a International Space Conference of Pacific-Basin Societies
|n (13th :
|d 2012 :
|c Kyoto, Japan)
|
| 245 |
1 |
0 |
|a Space for our future :
|b proceedings of the 13th International conference of Pacific-basin Societies (ISCOPS) held May 15-18 2012, Kyoto, Japan /
|c edited by Peter M. Bainum, Arun K. Misra, Yasuhiro Morita, Wang Jia.
|
| 264 |
|
1 |
|a San Diego, California :
|b Published for the American Astronautical Society by Univelt, Incorporated,
|c 2013.
|
| 264 |
|
4 |
|c ©2013
|
| 300 |
|
|
|a xvii, 823 pages :
|b illustrations ;
|c 25 cm.
|
| 300 |
|
|
|a 1 CD-ROM :
|b illustrations ;
|c 4 3/4 in..
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a unmediated
|b n
|2 rdamedia
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
|
|a volume
|b nc
|2 rdacarrier
|
| 338 |
|
|
|a computer disc
|b cd
|2 rdacarrier
|
| 490 |
1 |
|
|a Advances in the astronautical sciences,
|x 0065-3438 ;
|v v. 146
|
| 504 |
|
|
|a Includes bibliographical references and indexes.
|
| 505 |
0 |
|
|a The feasibiilty analysis of China cooperating with the U.S. in Mars exploration (AAS 12-511) -- Current and future space programs in Japan (AAS 12-512) -- Development and evaluation of a low-cost cots-based camera system for space applications (AAS 12-513) -- Minimum energy steering law for tacking maneuvers of satellites with CMGs (AAS 12-514) -- Optimal configuration of control moment gyros for minimum energy maneuvers of satellites (AAS 12-515) -- State estimation of planetary landing vehicles with wide-field integration of optic flow (AAS 12-516) -- Development of atomic number density measurement technique in hight enthalpy flows using vacuum ultraviolet absorption spectroscopy (AAS 12-517) -- Effect of Reynolds number and flow channel geometry on regression formula for forward-end faces in CAMUI type fuel grain (AAS 12-518) -- Orbit expressions in the continuous polar coordinate system (AAS 12-519) -- Study for direct measurement of electromagnetic thrust of electrodeless helicon plasma thruster (AAS 12-520) -- Electron cyclotron resonance plasma charging and acceleration of micro-particles for space thruster (AAS 12-521) -- Investigation on deflection behaviors of wrinkled membranes given by tension field theory (AAS 12-522) -- CARS measurement of rotational and vibrational temperatures on the flat plate behind shock wave (AAS 12-523) -- Development of strength failure model for porous charring layer of EPDM insulation eroded by particle flow (AAS 12-524) -- Important factors on receiver's measurement quality (AAS 12-525) --
|
| 505 |
0 |
|
|a Dynamics of a tether connected to an irregular shaped asteroid (AAS 12-526) -- Satellite constellation optimization method for future earth observation missions using small satellites (AAS 12-527) -- Hazard detection from high altitudes using a single camera (AAS 12-528) -- Probe measurement of plasma plume on electrodeless helicon plasma thruster using Lissajous acceleration (AAS 12-529) -- Immersion and invariance based command-filtered adaptive backstepping control of VTOL vehicles (AAS 12-530) -- Ignition investigation on a tri-fluid injector of hydrogen peroxide/kerosene (AAS 12-531) -- Flexible coupled dynamics modeling of variable configuration spacecraft oriented control (AAS 12-532) -- Near optimal deployment of a space elevator system (AAS 12-533) -- Equilibrium configurations and control of a moon-anchored tethered system (AAS 12-534) -- The athletic equation and stability of gyro-spacecraft with flexible accesory (AAS 12-535) -- Robotic autonomy in space: vision-based control of robotic capture operation (AAS 12-536) -- A study of the orbit determination for a spacecraft by using modified orbit estimator (AAS 12-537) -- Application of the formation flying analytical models to the Prisma Mission (AAS 12-538) -- A design of small circular halo orbits around the L2 of the Earth-Moon system (AAS 12-539) -- Trajectory design of Destiny Mission (AAS 12-540) --
|
| 505 |
0 |
|
|a Earth revolution synchronous orbits and aero-gravity assists to enhance capabilities for interplanetary missions by sub-payload spacecraft (AAS 12-541) -- Earth-Moon transfers involving periodic orbits and invariant manifolds through isomorphic mapping (AAS 12-542) -- The responsive and mobile concept of guidance and control system of Epsilon Rocket (AAS 12-543) -- Stability analysis of adaptive control based on characteristic model for the minimum-phase MIMO system (AAS 12-544) -- Performance evaluation for pointing control system for the balloon-borne telescope (AAS 12-545) -- The research on the key technique of the physics package of rubidium atomic clock (AAS 12-546) -- Detection peformance of upgraded "polished panel" optical receiver concept on the deep-space network's 34 meter research antenna (AAS 12-547) -- A software develoment and verification platform for on-board computers on small satellites (AAS 12-548) -- Fault-tolerant research of high performance soft-core processor based on FPGA (AAS 12-549) -- Design of an electrodynamic tether nanosatellite mission for space debris removal demonstration and radio science experiment (AAS 12-550) -- Small SAR satellite (AAS 12-551) -- Target detection by level set in digital processing of synthetic aperture radar (AAS 12-552) -- In-flight calibration for GOSAT TANSO (AAS 12-553) -- The use of onboard real-time dynamical compensation in high-accuracy image navigation of remote sensing satellite (AAS 12-554) -- Data collection micro satellite system task analysis and constellation design (AAS 12-555) -- HTV-R concept study (AAS 12-556) -- Study for the new usage of HTV (AAS 12-557) -- Commercial spaceports: the gateway for new space utilization (AAS 12-558) -- Influence of voids on the matrix of C/C composite (AAS 12-560) --
|
| 505 |
0 |
|
|a Development of carbon/carbon-silicon carbide composite for space mirrors (AAS 12-561) -- A vision of future space transportation systems (AAS 12-562) -- Research development and flight test of subscale winged rockets (AAS 12-563) -- Combustion characteristics of hybrid rocket motor using GAP-based solid fuel (AAS 12-565) -- Combustion mechanism and thruster application of HAN-based green propellant (AAS 12-566) -- Study on application of DBD plasma actuator for side force control of high-angle-of-attack slender body (AAS 12-567) -- Technical findings of HTV propulsion system associated with its dynamic characteristics (AAS 12-568) -- The development of HTV exposed pallet multi-purpose (AAS 12-569) -- Development of a hypersonic shock tube for planetary entry aerothermodynamics (AAS 12-570) -- Influence of elastic deformation on unsteady multi-body separation (AAS 12-571) --
|
| 505 |
0 |
|
|a Application of hte scaling technology in numerical study on the aerodynamic characteristics of launch vehicle (AAS 12-572) -- The development status of the Epsilon Launch Vehicle (AAS 12-573) -- Research and develoment progress of Space Transportation Propulsion R&D Center in JAXA (AAS 12-574) -- Overview of LE-X research and development program (AAS 12-575) -- Critical performance of trubopump mechanical elements for rocket engine (AAS 12-576) -- Development and test of the LOX/LNG regenerative cooled rocket engine (AAS 12-577) -- Pressure and geometry scaling of flowfield and combustion characteristics of gaseous hydrogen and gaseous oxygen shear-coaxial injectors (AAS 12-578) -- Post-flight analysis of Hayabusa; asteroid sample return capsule (AAS 12-579) -- Technical demonstrations for reusable sounding rocket system (AAS 12-580) -- Electrostatic levitation furance for the International Space Station (AAS 12-581) --
|
| 505 |
0 |
|
|a The study on structure of large reflector for space solar power systems (SSPS) (AAS 12-582) -- Exploring innovative ways of cooperation and technology transfer between Japan and Columbia (AAS 12-583) -- Destiny Mission overview: a small satellite mission for deep space exploration technology demonstration (AAS 12-585) -- Formation flying around libration points of circular restricted three body problem with small [mu] (AAS 12-586) -- Japanese Moon Lander SELENE-2 and its technology development (AAS 12-587) -- Launching low Mars Orbiter by using aerobraking (AAS 12-588) -- Error analysis and mid-course maneuver of Earth-Mars transfer orbit (AAS 12-589) -- On orbit design around a micro gravity asteroid (AAS 12-590).
|
| 650 |
|
0 |
|a Astronautics
|z Pacific Area
|x International cooperation
|v Congresses.
|
| 700 |
1 |
|
|a Bainum, Peter M.
|
| 773 |
1 |
8 |
|g no:146
|w 9937983420001701
|
| 830 |
|
0 |
|a Advances in astronautical sciences
|v v. 146.
|
| 999 |
1 |
0 |
|i 41fd20ce-508c-409c-a69f-1c7eb43bb931
|l 9915619500001701
|s US-MNU
|m space_for_our_futureproceedings_of_the_13th_international_conference_o_____2013_______publia________________________________________international_space________________e
|