Curriculum Vitaes

Junjiro Onoda

  (小野田 淳次郎)

Profile Information

Affiliation
Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Degree
Ph.D.(The University of Tokyo)

researchmap Member ID
1000144488

Research Interests

 2

Committee Memberships

 2

Papers

 122

Misc.

 42

Presentations

 247
  • 大久保洋志, 渡辺直行, 峯杉賢治, 小野田淳次郎, 高橋巧
    構造強度に関する講演会講演集, Jul 24, 2002
  • 槙原幹十朗, 小野田淳次郎
    構造強度に関する講演会講演集, Jul 24, 2002
  • 竹内伸介, 小野田淳次郎
    構造強度に関する講演会講演集, Jul 24, 2002
  • Koji Oya, Junjiro Onoda
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 2002
    Carpenter tape hinge made of TiNi alloy (a shape memory alloy) was designed, fabricated, and investigated. A carpenter tape hinge is one mechanism that has the advantages of high-reliability of deployment, lightweight, and low-cost. However, a traditional carpenter tape hinge has the disadvantage that a large shock arises when it springs into the deployed position. Our aim is to use TiNi alloy for a carpenter tape hinge instead of conventional spring materials. When the hinge is gradually heated, it deploys slowly under the resulting shape recovery force. And it deploys without a large latch shock. First, we determinated the configuration of the hinge that maximizes the stiffness. Next, we fabricated various configurations of hinges. We demonstrated deployment of the fabricated hinge and evaluate its characteristics through experiments and FEM analysis using ABAQUS. Moreover, we compared its characteristics with those of a conventional carpenter tape hinge and a plate-like hinge made of TiNi alloy through experiments and equations.
  • Hyun Ung Oh, Junjiro Onoda, Kenji Minesugi
    19th AIAA Applied Aerodynamics Conference, Dec 1, 2001
    This paper shows the effectiveness of a semiactive vibration isolator filled with liquid-crystal type electro-rheological (ER) fluid for disturbances generated by momentum-wheels. The principal characteristics of an ER isolator was measured in dynamic tests, and a mathematical model of the isolator was proposed. Two control laws for semiactive approach were proposed. Numerical simulation results indicated that the proposed semiactive control produced much better isolation performance than a passive system. © 2001 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
  • 槙原幹十朗, 小野田淳次郎
    構造強度に関する講演会講演集, Aug 1, 2001
  • OH H‐U, 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集, Aug 1, 2001
  • 大矢晃示, 小野田淳次郎
    構造強度に関する講演会講演集, Aug 1, 2001
  • 竹内伸介, 小野田淳次郎, 下瀬滋
    構造強度に関する講演会講演集, Aug 1, 2001
  • H. U. Oh, J. Onoda, K. Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 2001
    This paper shows the effectiveness of a semiactive vibration isolator filled with liquid-crystal type electro-rheological (ER) fluid for disturbances generated by momentum-wheels. The principal characteristics of an ER isolator was measured in dynamic tests, and a mathematical model of the isolator was proposed. Two control laws for semiactive approach were proposed. Numerical simulation results indicated that the proposed semiactive control produced much better isolation performance than a passive system.
  • H Uchida, J Onoda
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3, 2000, AMER INST AERONAUTICS & ASTRONAUTICS
    A formulation for simultaneously optimizing a passively damped structure and an active control system has been developed. A viscoelastic material (VERI) was utilized for enhancing passive damping of the structure. The formulation is applied to designing a free-free sandwich beam composed of three layers; that is, a simplified model of a beam-like space structure. The middle layer is made of the VEM in order to suppress elastic vibration modes passively. To stabilize the attitude and to actively suppress the elastic vibration modes, an active attitude-controller is mounted on the structure. The optimized costs indicate that optimization of the viscous passive damping is useful not only for reducing total system cost of the structure and the active controller but also for improving stability robustness of the closed-loop system.
  • H Uchida, J Onoda
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3, 2000, AMER INST AERONAUTICS & ASTRONAUTICS
    A formulation for simultaneously optimizing a passively damped structure and an active control system has been developed. A viscoelastic material (VERI) was utilized for enhancing passive damping of the structure. The formulation is applied to designing a free-free sandwich beam composed of three layers; that is, a simplified model of a beam-like space structure. The middle layer is made of the VEM in order to suppress elastic vibration modes passively. To stabilize the attitude and to actively suppress the elastic vibration modes, an active attitude-controller is mounted on the structure. The optimized costs indicate that optimization of the viscous passive damping is useful not only for reducing total system cost of the structure and the active controller but also for improving stability robustness of the closed-loop system.
  • 内田英樹, 小野田淳次郎
    日本機械学会スペース・エンジニアリング・コンファレンス講演論文集, Nov 24, 1999
  • 竹内伸介, 小野田淳次郎
    構造強度に関する講演会講演集, Jul 14, 1999
  • 清水さやか, 大久保洋志, 渡辺直行, 峯杉賢治, 小野田淳次郎
    構造強度に関する講演会講演集, Jul 14, 1999
  • Hyun Ung Oh, Junjiro Onoda
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 1999
    To semiactively suppress the vibration of space truss structure, a variable damper was fabricated with liquid-quartz, which was a type of ER fluid. The principal characteristics of a liquid-quartz variable damper were measured in quasi-static tests, and a simple mathematical model of the damper was proposed. Based on the mathematical model of the damper and the LQR theory, two kinds of semiactive on-off control laws were proposed. The effectiveness of the semiactive vibration suppression with the liquid-quartz type ER fluid variable damper was investigated by numerical simulations in comparison with a particle-dispersion type ER fluid variable damper which was previously fabricated and tested by Onoda et al.1. Simulation results indicated that the most of the proposed control laws result in much higher performances than that of optimally tuned passive system, and simulation results also demonstrated that the liquid-quartz type ER fluid variable damper were superior to the particle-dispersion type ER fluid variable damper from the view point of amplitude-dependence. Semiactive vibration suppression experiments of a ten bay truss beam with the liquid-quartz ER fluid variable damper were also performed, and the experiment results also demonstrated that vibration was suppressed nicely.
  • 東海林和典, 菊池忠彦, 竹井秀樹, 梅里真弘, 峯杉賢治, 小野田淳次郎
    宇宙科学技術連合講演会講演集, Oct, 1998
  • 小野田淳次郎
    日本機械学会通常総会講演会講演論文集, Mar, 1998
  • 上田光幸, 小野田淳次郎
    構造強度に関する講演会講演集, 1998
  • 竹中達史, 小野田淳次郎
    構造強度に関する講演会講演集, 1998
  • OH H, 小野田淳次郎
    構造強度に関する講演会講演集, 1998
  • 沼尻至朗, 小野田淳次郎
    構造強度に関する講演会講演集, 1998
  • 小野田淳次郎, 峯杉賢治, 中村正俊, 柳沢昇
    構造強度に関する講演会講演集, 1998
  • 高野敦, 小野田淳次郎
    構造強度に関する講演会講演集, 1998
  • Junjiro Onoda, Hyun Ung Oh, Kenji Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 1998
    This paper proposes and investigates a method to enhance ER-fluid variable dampers for semiactive vibration suppression. The ER-fluid dampers studied in this paper can be modeled as a variable friction damper. The friction in the damper is an increasing function of the absolute value of the voltage applied to the electrode of the damper. Generally, the friction is not zero even when no voltage is applied. Semiactive vibration suppression is to control the friction such that vibrations damp quickly. Therefore, to suppress large amplitude vibrations to small amplitude, the friction needs to be varied through a large range. In other word, the ratio of the maximum and minimum values of the frictional force needs to be large. To increase the ratio by decreasing the minimum frictional force, this paper proposes to excite a high-frequency vibration of the electrode. The effectiveness of the electrode vibration for the reduction of the minimum frictional force is demonstrated in this paper by both static experiments and semiactive vibration suppression experiments. The results of semiactive vibration suppression experiments indicate that the minimum frictional force is reduced by the electrode vibration by factor of 1/3-1/2.
  • Hideki Uchida, Junjiro Onoda
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 1998
    A formulation of simultaneous optimization a passively damped structure and active controller has been attempted. In this study, viscoelastic materials (VEMs) have been utilized as one of device to enhance damping passively. The formulation needs to adopt the modeling method that is capable of designing not only the viscous passive damping but also the active controller adequately. For such requirement, the time domain approach that results the accurate model on the time domain is employed for the modeling of the viscoelastic structures. In order to create the reduced order model (ROM) for system design, the complex modal analysis has been developed, and the ROM is obtained with using both truncation and the balanced realization method. The accuracy of the ROM has been investigated based on a cantilevered partially viscoelastic beam example. The numerical results indicate that the time domain approach is more appropriate than the modal strain energy (MSE) method for creation of the ROM. Moreover, the strategy to derive the ROM is included into the formulation of simultaneous optimization of a viscoelastic structure and active controller. The formulation is applied to the design of a sandwich beam like space structure. The optimization results indicate that the optimization of viscous passive damping is useful for the total system cost reduction.
  • 小野田淳次郎, 峯杉賢治, 竹内伸介
    構造強度に関する講演会講演集, 1997
  • 小野田淳次郎, 栗林一彦, 峯杉賢治, 西田稔夫
    構造強度に関する講演会講演集, 1997
  • 小野田淳次郎, 峯杉賢治
    構造強度に関する講演会講演集, 1997
  • 小野田淳次郎, 峯杉賢治, 中村正俊, 柳沢昇
    構造強度に関する講演会講演集, 1997
  • 小野田淳次郎, 峯杉賢治, 大塚秀和
    構造強度に関する講演会講演集, 1997
  • 内田英樹, 小野田淳次郎
    構造強度に関する講演会講演集, 1997
  • 上田光幸, 小野田淳次郎
    日本機械学会通常総会講演会講演論文集, Apr, 1996
  • 小野田淳次郎, OH H‐U
    日本機械学会通常総会講演会講演論文集, Apr, 1996
  • 小野田淳次郎, 内田英樹
    日本機械学会通常総会講演会講演論文集, Apr, 1996
  • 戸田勧, 木部勢至朗, 杉本直, 河島信樹, 矢守章, 小野田淳次郎
    スペース・プラズマ研究会, Mar, 1996
  • 小野田淳次郎, 峯杉賢治, 竹内伸介
    構造強度に関する講演会講演集, 1996
  • 上田光幸, 小野田淳次郎
    構造強度に関する講演会講演集, 1996
  • 大久保洋志, 峯杉賢治, 小野田淳次郎, 渡辺直行
    構造強度に関する講演会講演集, 1996
  • 小野田淳次郎, 峯杉賢治, OH H U
    構造強度に関する講演会講演集, 1996
  • 荒井貴, 関根功治, 田中隆吉, 小野田淳次郎
    飛行機シンポジウム講演集, 1996
  • 森章, 上田光幸, 内田英樹, 竹内伸介, 小野田淳次郎
    構造強度に関する講演会講演集, 1996
  • Kenji Minesugi, Junjiro Onoda, Hiroshi Ohkubot, Yoji Hanawa
    37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1996, American Institute of Aeronautics and Astronautics Inc, AIAA
    Passive damping augmentation is one of the effective method for vibration suppression because it is definitely stable and generally simple. Thin film with viscous lamina showed a remarkable effect for passive vibration suppression in the practical application to a satellite. To investigate its damping capability, several kinds of experiments have been performed. The results show that the non-linear relation between shear load and shear deformation velocity in the viscous lamina of the thin film contributes to the damping capability. Simple mathematical model is made to represent the behavior of the film.
  • Junjiro Onoda, Hyun-Ung Oh, Kenji Minesugi
    37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1996, American Institute of Aeronautics and Astronautics Inc, AIAA
    To semiactively suppress the vibration of space truss structures, a variable damper using Electro- Rheological (ER) fluid is designed and fabricated. The characteristics of the damper are measured, and a simple mathematical model of the damper is proposed. Based on this mathematical model, several semiactive control laws are proposed for vibration suppression of multiple degree- of-freedom (MDOF) structures with multiple dampers. To investigate the performances of the scheme, numerical simulations of semiactive vibration suppression of a ten-bay truss beam with ER fluid dampers are performed. Simulation results indicate that the most of the proposed semiactive control laws result in much higher performances than that of the optimally tuned passive system. A semiactive vibration suppression experiment of the ten-bay truss beam with the ER fluid damper is also performed. The experiment results also demonstrate the effectiveness of the scheme for the actual MDOF structure.
  • Hideki Uhicda, Junjiro Onoda
    37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference, 1996, American Institute of Aeronautics and Astronautics Inc, AIAA
    This paper discusses that optimal design of passive damping is effective for performance improvement on the simultaneous structure/controller optimization problem for flexible space structures. In this study, structural passive damping is assumed to viscous passive damping, and the simultaneous optimization of active controller gains, structural stiffness, and viscous passive damping elements is performed. In order to control lower modes, the Linear Quadratic Gaussian (LQG) controller is adopted. Besides, in order to damp residual modes actively, the Direct Velocity Feedback (DVFB) controller, whose function is similar to viscous passive damping elements, is adopted. In this paper, effects of the quality of the DVFB controller are also investigated. As one of typical numerical examples, a controlled simply supported sandwich beam structure that has a viscoelastic layer is investigated. Through the observation of the numerical results, it is confirmed that the optimal design of the viscous damping elements is useful for the performance improvement on the simultaneous optimization of the structure and the control system.
  • OH H‐U, 小野田淳次郎
    宇宙科学技術連合講演会講演集, Oct, 1995
  • 内田英樹, 小野田淳次郎
    宇宙科学技術連合講演会講演集, Oct, 1995
  • 樋口健, 小野田淳次郎, 峯杉賢治, 芝山有三, 東海林和典, 菊池忠彦, 大賀弘一
    宇宙科学技術連合講演会講演集, Oct, 1995
  • Junjiro Onoda, Dan Ying Fu, Kenji Minesugi
    Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Jan 1, 1995
    A two-dimensionally deployable truss structure is newly proposed for space application, whose most significant feature is its small number of mechanisms to be locked when it is deployed. Its packaging efficiency is shown to be better than many known deployable trusses. Several versions of the truss are also proposed. To confirm that the new deployable truss has enough design flexibility, a paraboloidal truss platform is designed for trial. Furthermore, a numerical investigation shows that the platform is actually deployable/foldable from the practical point of view.

Research Projects

 12