Catalog

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1. Sameshima S., Kawakatsu Y.,
gStudy on Low-Cost System Configuration for Earth-Moon Transportationh,
Advances in the Astronautical Sciences,
Vol. 77, pp. 663-675, AAS 91-606, 1991.


2. Kawakatsu Y., Yamada K.,
gHeuristic Approach to Launch Vehicle Trajectory Designh,
Proceedings of the 18th International Symposium on Space Technology and Science,
pp. 2487-2495, 1992.


3. Kawakatsu Y., Watanabe T.,
gFeasibility Study on Enhancement of OTV Capability by Tether for Orbital Transfer Operationsh,
Proceedings of the 19th International Symposium on Space Technology and Science,
pp. 553-560, 1994.


4. Kawakatsu Y., Watanabe T., Nakasuka S.,
gOrbital Transfer Operation Utilizing Rotational Motion of Tetherh,
Proceedings of the 4th Workshop on Astrodynamics and Flight Mechanics,
pp. 93-98, 1994.


5. Nakasuka S., Kawakatsu Y., Ninomiya T., et al.,
gStudy on the Relative Motion and Orbit Design for Clustered Satelliteh,
Proceedings of the 4th Workshop on Astrodynamics and Flight Mechanics,
pp. 88-92, 1994.


6. Kawakatsu Y.,
gEfficient Design of Launch Vehicle Trajectory Utilizing Design Knowledgeh,
The 45th International Astronautical Congress,
ST-94-562, 1994.


7. Kawakatsu Y., Watanabe T., Nakasuka S.,
gStudy on Rotational Motion of Dumbbell Shaped Rigid Body on Elliptical Orbith,
Proceedings of the 5th Workshop on Astrodynamics and Flight Mechanics,
pp. 247-252, 1995.


8. Kawakatsu Y., Kaneko Y., Takizawa Y.,
gTrajectory Design of SELENE Lunar Orbiting and Landingh,
Advances in the Astronautical Sciences,
Vol. 100, pp. 269-280, AAS 98-320, 1998.


9. Kawakatsu Y., Nakasuka S.,
gRotational Motion of Rigid Body on Elliptical Orbith,
Proceedings of the 2nd International Conference on Nonlinear Problems in Aviation & Aerospace,
pp. 357-364, 1998.


10. Kawakatsu Y., Kinoshita T., Takizawa Y.,
gGuidance, Navigation, Control of SELENE Lunar Landing Missionh,
Proceedings of the 2nd International Conference on Nonlinear Problems in Aviation & Aerospace,
pp. 349-356, 1998.


11. Kawakatsu Y., Kaneko Y., Takizawa Y.,
gDesign of Translunar Trajectory and Relay Satellite Orbit of SELENEh,
Proceedings of the 21st International Symposium on Space Technology and Science,
pp. 1475-1480, 1998.


12. Nakasuka S., Nagashima R., Kawakatsu Y., et al.,
gNon Critical Spacecraft System - A Novel Concept for Spacecraft Design Using Hyper Redundancyh, Proceedings of the 21st International Symposium on Space Technology and Science,
pp. 980-985, 1998.


13. Motohashi S., Nakasuka S., Aoki T., Narusawa Y., Nagashima R., Kawakatsu Y., et al.,
gOn-orbit Dynamics and New Control Scheme for Large Membrane "Furoshiki" Satelliteh,
Proceedings of the 21st International Symposium on Space Technology and Science,
pp. 1072-1077, 1998.


14. Narusawa Y., Aoki T., Nakasuka S., Motohashi S., Nagashima R., Kawakatsu Y., et al.,
gBehavior of Membrane Structures under Microgravity Environmentg,
Proceedings of the 21st International Symposium on Space Technology and Science,
pp. 428-433, 1998.


15. Nagashima R., Nakasuka S., Kawakatsu Y.,
gThe Preliminary Study on the Effective Utilization of a Lunar-Derived Propellant (LOX)h,
The 49th International Astronautical Congress, IAA-98-IAA.13.2.07, 1998.


16. Kawakatsu Y., Kaneko Y., Takizawa Y., et al.,
gSELENE Translunar Trajectory and Lunar Orbit Injectionh,
The 14th International Symposium on Space Flight Dynamics, 1999.


17. Kawakatsu Y., TakizawaY., Kaneko Y., et al.,
gApplication of Phasing Orbit on SELENE Translunar Trajectoryh,
Proceedings of the 22nd International Symposium on Space Technology and Science,
pp. 1570-1575, May 2000.


18. Ninomiya T., Hamada Y., Sasa S., Yamaguchi I., Hikida S., Kaneko Y., Kawakatsu Y., et al.,
gSELENE Model-Following System Using Flying Test Bedh,
Proceedings of the 22nd International Symposium on Space Technology and Science,
pp. 1594-1599, 2000.


19. Ueno S., Asaba K., Kawakatsu Y.,
gMinimum-Fuel Interplanetary Trajectories Using Solar Electric Propulsionh,
AIAA/AAS Astrodynamics Specialist Conference, 2000.


20. Nakasuka S., Aoki T., Ikeda I., Tsuda Y., Kawakatsu Y.,
g"Furoshiki Satellite" ? a Large Membrane Structure as a Novel Space Systemh,
The 51st International Astronautical Congress, IAF 00-U101, 2005.

21. Nakasuka S., Tsuda Y., Eishima T., Kawakatsu Y., et al.,
gTwo New Spacecraft Architectures and Their Impacts on Electric Propulsionh,
The 26th Internatioal Electric Propulsion Conference, 2000.


22. Nakazawa S., Kawakatsu Y., Nagae Y., et al.,
gSystem Design and the Status of SELENEh,
Proceedings of the 23th International Symposium on Space Technology and Science,
pp. 1910-1915, 2002.


23. Kawakatsu Y., Sasaki S., Takizawa Y.,
gSystem Level Investigation Example in SELENE Spacecraft Designh,
Proceedings of the 24th International Symposium on Space Technology and Science,
pp. 1092-1102, 2004.

24. Kamiya T., Kurii T., Kawakatsu Y.,
gMicrovibration Management and Pointing Stability Analysis of SELENE Satelliteh,
The 16th IFAC Symposium on Automatic Control in Aerospace, 2004.


25. Yano T., Goda N., Yamada Y., Kawakatsu Y.,
gDetermination of the Positions of Stars with High Accuracy for JASMINEhC
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 158-163, 2004.


26. Kawakatsu Y.
gStudy on the Characteristics of Two-Burn Translunar TrajectoryhC
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 294-299, 2004.


27. Kamiya T., Kurii T., Kawakatsu Y.,
gSELENE Microvibration Management Synthesis for Achievement of Pointing StabilityhC
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 181-187, 2004.


28. Yamakawa H., Kawakatsu Y., Abe M.,
gMultiple Near-Earth Asteroid Sample Return Mission in the Next Decade: Preliminary Designh,
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 193-199, 2004.


29. Kawakatsu Y.C Yamakawa H., Abe M.,
gPreliminary Study on the Orbit Planning of Near-Earth Asteroid Multiple Sample Return Missionh
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 200-205, 2004.


30. Matsumoto M., Kawakatsu Y.,
gPreliminary Mission Design for Main-belt Asteroids Multi-Flybys Explorationh,
Proceedings of the 14th Workshop on Astrodynamics and Flight Mechanics,
pp. 206-211, 2004.


31. Yamakawa H., Kawakatsu Y., Morimoto M., et al.,
gLow-thrust Trajectory Design for a Low-cost Multiple Asteroid Rendezvous and Sample Return Missionh,
The 55th International Astronautical Congress, IAC-04-Q.P.20, 2004.


32. Kawakatsu Y., gStudy on the Characteristics of Two-burn Translunar Trajectoryh,
Proceedings of the 18th International Symposium on Space Flight Dynamics (ESA-SP-548),
pp. 239-244, 2004.


33. Aida S., Matsumoto M., Kawakatsu Y., et al.,
gOptimization of Trajectories between the Earth to the L2 Pointh,
Proceedings of the 15th Workshop on Astrodynamics and Flight Mechanics,
pp. 18-22, 2005.


34. Tarao K., Mori O., Kawakatsu Y., et al.,
gAnalysis of Autonomous Optical Guidance and Navigation Strategy during Flyby",
Proceedings of the 15th Workshop on Astrodynamics and Flight Mechanics,
pp. 413-417, 2005.


35. Kawakatsu Y., Yamakawa H., Abe M.,
gTrajectory Analysis of Post-Hayabusa Asteroid Explorer Missionh,
Proceedings of the 15th Workshop on Astrodynamics and Flight Mechanics,
pp. 135-140, 2005.


36. Kawakatsu Y., Mori O.,
gMission Analysis of Asteroid Flyby Exploration by Miniature Asteroid Interceptorsh,
Proceedings of the 15th Workshop on Astrodynamics and Flight Mechanics,
pp. 141-146, 2005.


37. Fujiwara A., Abe M., Kawakatsu Y., , et al.,
gStudy of Post-Hayabusa Sample Return Mission to Primitive Type Asteroidsh,
Proceedings of the 6th International Conference on Low-Cost Planetary Missions,
pp. 133-136, 2005.


38. Kawakatsu Y., Mori O., Tsuda Y., et al.,
gMission Concept of Multiple Near Earth Asteroids Exploration by Miniature Asteroid Interceptorsh
Proceedings of the 6th International Conference on Low-Cost Planetary Missions,
pp. 145-152, 2005.


39. Mori O., Kawakatsu Y., Tarao K., et al.,
gThe System and Integrated Guidance and Navigation Strategy of Asteroid Interceptorsh,
Proceedings of the 6th International Conference on Low-Cost Planetary Missions,
pp. 201-208, 2005.


40. Mori O., Tarao K., Kawakatsu Y., et al.,
gMission Design and Integrated Guidance and Navigation Strategy for NEO Flyby Using eInterceptorfh,
The 56th International Astronautical Congress, IAC-05-B5.2.04, 2005.


41. Kawakatsu Y.,
gConcept Study on Deep Space Orbit Transfer Vehicleh,
The 56th International Astronautical Congress, IAC-05-D2.3.07, 2005.

42. Kawakatsu Y., Mori O., Tsuda Y., et al., gMission Analysis of Multiple Near Earth Asteroids Exploration by Miniature Asteroid Interceptorsh, Advances in the Astronautical Sciences, Vol. 124, pp. 1773-1787, AAS 06-212, 2006.

43. Gouda N., Kobayashi Y., Yamada Y., Yano T., Tsujimoto T., Suganuma M., Niwa Y., Yamauchi M., Kawakatsu Y., et al.,
gJASMINE: Galactic Structure Surveyorh,
Proceedings of SPIE ? The International Society for Optical Engineering,
p626542, 2006.


44. Matsumoto S., Takizawa Y., Konishi H., Yamamoto M., Iwana Y., Ogawa M., Kawakatsu Y.,
gLunar Transfer Orbit for SELENEh,
Proceedings of the 19th International Symposium on Space Flight Dynamics,
pp. 506-511, 2006.


45. Kawakatsu Y., Yamamoto M., Kawaguchi J.,
gStudy on the Lunar Approach Strategies Tolerant of Lunar Orbit Injection Failureh,
Proceedings of the 19th International Symposium on Space Flight Dynamics,
pp. 575-580, 2006.


46. Aida S., Kawakatsu Y., Kawaguchi J., et al.,
gOptimization of Trajectories from Earth to L2h,
The 19th International Symposium on Space Flight Dynamics, ISTS 2006-d-66, 2006.


47. Abe M., Kawakatsu Y., Yano H., et al.,
gThe Minor Body Sample Return Mission in the Post-Hayabusa Erah,
Proceedings of the 25th International Symposium on Space Technology and Science,
pp. 1062-1065, 2006.


48. Kawakatsu Y., Yamamoto M., Kawaguchi J.,
gRobust Lunar Orbit Injection using the Moon Synchronous Orbith,
Proceedings of the 16th Workshop on Astrodynamics and Flight Mechanics,
pp. 55-60, 2006.


49. Arakawa M., Kawakatsu Y.,
gStudy on the Back-up Sequence of Translunar Trajectoryh,
Proceedings of the 16th Workshop on Astrodynamics and Flight Mechanics,
pp. 61-65, 2006.


50. Kawakatsu Y., Hashimoto T., Bando N., et al.
gInitial Phase AOCS Operation of Infrared Astronomy Satellite eAKARIfh,
Proceedings of the 16th Workshop on Astrodynamics and Flight Mechanics,
pp. 215-220, 2006.


51. Kawakatsu Y., Abe M., Kawaguchi J.,
gMission Analysis of the Sample Return from Primitive Type Near Earth Asteroidh,
Advances in the Astronautical Sciences,
Vol. 127, pp. 2119-2131, AAS 07-246, 2007.


52. Kawakatsu Y., Hashimoto T., Bando N.,
gInitial Phase AOCS Operation of Infrared Astronomy Satellite eAKARIfh,
The 30th Annual AAS Guidance and Control Conference, AAS 07-092, 2007.


53. Kawakatsu Y., Abe M., Kawaguchi J.,
gMission Analysis of Hayabusa2, the Next Japanese Asteroid Exploration Missionh,
The 17th Workshop on Astrodynamics and Flight Mechanics, 2007.


54. Kawakatsu Y.,
gTranslunar Trajectory Reconfiguration for the Case of Main Engine Anomalyh,
The 17th Workshop on Astrodynamics and Flight Mechanics, 2007.


55. Okada S., Shirasawa Y., Miwa Y., Mori O., Kawakatsu Y., et al.,
gDesign of Attitude Control System for H2A Piggyback Solar Sail Spacecrafth,
The 17th Workshop on Astrodynamics and Flight Mechanics, 2007.


56. Matsumoto M., Funase R., Tsuda Y., Kawakatsu Y.,
gAttitude Determination of Spin Stabilized Micro Spacecraft Using RF Doppler Measurementsh,
The 17th Workshop on Astrodynamics and Flight Mechanics, 2007.


57. Kawakatsu Y.,
gSELENE Translunar Trajectory Reconfiguration Plan Provided for the Case of Main Engine Anomalyh,
The 20th International Symposium on Space Flight Dynamics, 2007.


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