Research Career 【 display / non-display 】

Research Career 【 display / non-display 】

• Optimal control of aircrafts

  Project Year：  -   

• Attitude control of satellites

  Project Year：  -   

• Optimal guidance and control of manipulators

  Project Year：  -   

• Optimum trajectory design for planetary explorer

  Project Year：  -   

Papers 【 display / non-display 】

Papers 【 display / non-display 】

• A Proposal for Regional Division and Index of Choosing Agent Number by Heterogeneous Multiagent System with Multiplicatively Weighted Voronoi Tessellation

  ICHIHARA Kisho, UENO Seiya

  Transactions of the Society of Instrument and Control Engineers ( The Society of Instrument and Control Engineers )  57 ( 3 )   120 - 127   2021

  Joint Work

  　View Summary

  <p>This paper describes a partitioning method of region and index of choosing number for heterogeneous swarm of unmanned vehicles using multiplicatively weighted Voronoi tessellation and simple formulation. Although recent researches have verified the effectiveness of swarm of unmanned vehicles at the time of natural disaster etc. and many researches related to them have been made, most of them are homogeneous swarm. On the other hand, there are few researches related to heterogeneous swarm because of their complexity and difficulty of generalizing and formulating models. This paper proposes the method of generalizing heterogeneous swarm model and partitioning method of searching region which is one of the most possible missions for them. In this paper, Voronoi tessellation in computational geometry has been applied which is one of the representative partitioning methods in general.</p>

  DOI CiNii

• Control of Tracking Network for Real UGVs with Disturbance

  KATA Hiroaki, UENO Seiya, DOBASHI Junya

  Transactions of the Society of Instrument and Control Engineers ( The Society of Instrument and Control Engineers )  56 ( 3 )   81 - 88   2020

  Joint Work

  　View Summary

  <p>Communication network formation and position control law for multiple unmanned ground vehicles (UGVs) to monitor a moving target at base station is proposed. A monitoring image of the target that acquired by nearby UGV is sent to base station through the communication network. Each UGV forms a communication network and calculates own moving amount with virtual forces using only information in local area. Since an error occurs in movement of real UGV, modified position control law is introduced. Numerical simulation and experiments show the effectiveness of this control law.</p>

  DOI CiNii

• Control Law of Target Tracking for Multiple Autonomous UAVs Using Virtual Forces

  KATA Hiroaki, UENO Seiya

  Transactions of the Society of Instrument and Control Engineers ( The Society of Instrument and Control Engineers )  55 ( 3 )   189 - 196   2019

  Joint Work

  　View Summary

  <p>Position control law for multiple unmanned aerial vehicles (UAVs) to monitor a moving target using virtual forces is proposed. A monitoring image of the target that acquired by a nearby UAV is sent to base through the UAVs network. Each UAV forms a communication network and calculates own moving amount with a virtual forces using only information in local area. Numerical simulations show that the proposed control law is valid.</p>

  DOI CiNii

• Motion estimation of a stalled aircraft based on image processing

  SAITO YUTA, HIGUTI TAKEHIRO, UENO SEIYA, NAGASAKI FUMINAO

  Proceedings of the Japan Joint Automatic Control Conference ( The Japan Joint Automatic Control Conference )  61 ( 0 )   1708 - 1712   2018

  Joint Work

  DOI CiNii

• Optimal Trajectory of Powered Descending Phase with Coasting for Smart Lander for Investigating Moon

  HIGUCHI Takehiro, UENO Seiya, KIMURA Yuuta

  AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ( THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES )  17 ( 0 )   55 - 60   2018

  Joint Work

  　View Summary

  <p>This paper is on optimal trajectory of future lunar lander with coasting in powered descending phase. For the light weight/low cost lunar lander, optical navigation using onboard cameras to identify their current state is one of very few techniques available to achieve the pin-point landing. The optical navigation is to be operated between the powered descending phases, when the orbital maneuvering engine (OME) is turned off. This paper shows the series of different coasting conditions and discusses the effect of the coasting to the trajectory and fuel consumption. The results give some ideas for future gravitational planetary missions, which uses coasting during their powered descending phase. In addition, optimal trajectory with double coasting for the SLIM project is shown in this paper.</p>

  DOI CiNii

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Review Papers 【 display / non-display 】

Review Papers 【 display / non-display 】

• JSASS Space Vision 2050

  UENO Seiya, HIRAKO Keiichi, MIZUNO Motoko, IMAMURA Taro, FUNAKI Ikkoh, KIKUCHI Koichi

  Aeronautical and Space Sciences Japan ( THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES )  67 ( 8 ) 269 - 274   2019.08  [Refereed]  [Invited]

  Introduction and explanation (scientific journal)   Joint Work

  　View Summary

  <p>A half century has passed since Japan Society for Aeronautical and Space Sciences (JSASS) was renamed in the official Japanese name. The previous name was the Japan Society of Aeronautical Engineering. It can be said that this half century is the history of Japanese space engineering and sciences. The board of directors of JSASS decided to publish 'JSASS Space Vision 2050' for the future space activities. JSASS Space Vision 2050 consists of 'Space vision' and 'Space roadmaps.' 'Space vision' shows expected space activities in 2050 and the future, and 'Space roadmaps' show technical and political items to be cleared by 2030 and 2040.</p>

  DOI

• Control Technology Used in Aerospace

  UENO Seiya, ICHIKAWA Tsutomu

  Journal of The Society of Instrument and Control Engineers ( The Society of Instrument and Control Engineers )  57 ( 4 ) 212 - 213   2018.04  [Refereed]  [Invited]

  Introduction and explanation (scientific journal)   Joint Work

  DOI

• Reliability of Control System in Aerospace Field

    30 ( 5 ) 386 - 391   2008.07

  Introduction and explanation (scientific journal)   Single Work

Grant-in-Aid for Scientific Research 【 display / non-display 】

Grant-in-Aid for Scientific Research 【 display / non-display 】

• Grant-in-Aid for Scientific Research(B)

  Project Year： 2016.04  -  2019.03 

• Grant-in-Aid for challenging Exploratory Research

  Project Year： 2016.04  -  2019.03 

Preferred joint research theme 【 display / non-display 】

Preferred joint research theme 【 display / non-display 】