Catalog

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1. Sameshima S., Kawakatsu Y.,
gStudy on Low-Cost System Configuration for Earth-Moon Transportationh,
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 Designh,
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 Operationsh,
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 Tetherh,
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 Satelliteh,
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 Knowledgeh,
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 Orbith,
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 Landingh,
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 Orbith,
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 Missionh,
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 SELENEh,
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 Redundancyh, 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" Satelliteh,
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 Environmentg,
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 Injectionh,
The 14th International Symposium on Space Flight Dynamics, 1999.


17. Kawakatsu Y., TakizawaY., Kaneko Y., et al.,
gApplication of Phasing Orbit on SELENE Translunar Trajectoryh,
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 Bedh,
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 Propulsionh,
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 Systemh,
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 Propulsionh,
The 26th Internatioal Electric Propulsion Conference, 2000.


22. Nakazawa S., Kawakatsu Y., Nagae Y., et al.,
gSystem Design and the Status of SELENEh,
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 Designh,
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 Satelliteh,
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 JASMINEhC
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 TrajectoryhC
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 StabilityhC
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 Designh,
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 Missionh
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 Explorationh,
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 Missionh,
The 55th International Astronautical Congress, IAC-04-Q.P.20, 2004.


32. Kawakatsu Y., gStudy on the Characteristics of Two-burn Translunar Trajectoryh,
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 Pointh,
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 Missionh,
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 Interceptorsh,
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 Asteroidsh,
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 Interceptorsh
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 Interceptorsh,
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 eInterceptorfh,
The 56th International Astronautical Congress, IAC-05-B5.2.04, 2005.


41. Kawakatsu Y.,
gConcept Study on Deep Space Orbit Transfer Vehicleh,
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 Interceptorsh, 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 Surveyorh,
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 SELENEh,
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 Failureh,
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 L2h,
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 Erah,
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 Orbith,
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 Trajectoryh,
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 eAKARIfh,
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 Asteroidh,
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 eAKARIfh,
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 Missionh,
The 17th Workshop on Astrodynamics and Flight Mechanics, 2007.


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


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


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