Research Output 1983 2019

2019

Controllability analysis of propellant-free satellite formation flight

Shouman, M., Bando, M. & Hokamoto, S., Jan 1 2019, Spaceflight Mechanics 2019. Topputo, F., Sinclair, A. J., Wilkins, M. P. & Zanetti, R. (eds.). Univelt Inc., p. 3577-3596 20 p. AAS 19-384. (Advances in the Astronautical Sciences; vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

controllability
propellants
Propellants
Controllability
flight

Integrated orbit determination and maintenance in Earth-Moon unstable dynamics environment

Zhou, Y., Bando, M., Hokamoto, S. & Wu, P., Oct 1 2019, In : Acta Astronautica. 163, p. 69-76 8 p.

Research output: Contribution to journalArticle

Moon
Orbits
Earth (planet)
Spacecraft
Covariance matrix

Output regulation control for satellite formation flying using differential drag

Shouman, M., Bando, M. & Hokamoto, S., Jan 1 2019, In : Journal of Guidance, Control, and Dynamics. 42, 10, p. 2220-2232 13 p.

Research output: Contribution to journalArticle

Formation Flying
Output Regulation
formation flying
Drag
drag

Output regulation control for satellite formation flying using differential drag

Shouman, M., Bando, M. & Hokamoto, S., Jan 1 2019, Spaceflight Mechanics 2019. Topputo, F., Sinclair, A. J., Wilkins, M. P. & Zanetti, R. (eds.). Univelt Inc., p. 3433-3452 20 p. AAS 19-307. (Advances in the Astronautical Sciences; vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

formation flying
drag
Drag
Satellites
Aerodynamic drag

Periodic and quasi-periodic orbit design based on the center manifold theory

Akiyama, Y., Bando, M. & Hokamoto, S., Jul 1 2019, In : Acta Astronautica. 160, p. 672-682 11 p.

Research output: Contribution to journalArticle

Orbits
Sun
Numerical methods
Earth (planet)

Sparse optimal trajectory design in three-body problem

Kayama, Y., Bando, M. & Hokamoto, S., Jan 1 2019, Spaceflight Mechanics 2019. Topputo, F., Sinclair, A. J., Wilkins, M. P. & Zanetti, R. (eds.). Univelt Inc., p. 2599-2618 20 p. AAS 19-359. (Advances in the Astronautical Sciences; vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

three body problem
trajectory
Trajectories
trajectories
dynamical systems

Trajectory design in the circular restricted three-body problem using artificial invariant manifolds

Oshima, Y., Bando, M. & Hokamoto, S., Jan 1 2019, Spaceflight Mechanics 2019. Topputo, F., Sinclair, A. J., Wilkins, M. P. & Zanetti, R. (eds.). Univelt Inc., p. 1235-1254 20 p. AAS 19-396. (Advances in the Astronautical Sciences; vol. 168).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

three body problem
Orbits
spacecraft
trajectory
Trajectories
2018
Open Access
Attitude control
Position control
Deceleration
Motion planning
Controllers

Controller performance for quad-rotor vehicles based on sliding mode control

Oba, T., Bando, M. & Hokamoto, S., Jun 1 2018, In : Journal of Robotics and Mechatronics. 30, 3, p. 397-405 9 p.

Research output: Contribution to journalArticle

Sliding mode control
Rotors
Controllers
Feedback
Control systems
1 Citation (Scopus)

Explicit form of station-keeping and formation flying controller for libration point orbits

Yuki, A., Bando, M. & Hokamoto, S., Jan 1 2018, In : Journal of Guidance, Control, and Dynamics. 41, 6, p. 1405-1413 9 p.

Research output: Contribution to journalArticle

Formation Flying
formation flying
libration
Output Regulation
controllers
three body problem
design method
libration
Orbits
trajectory
2 Citations (Scopus)
Unmanned aerial vehicles (UAV)
Motion planning
Evolutionary algorithms
Demonstrations
Collision avoidance

Flight test results of parafoil-type vehicle with inflatable structure for the martian exploration

Moriyoshi, T., Yamada, K., Higashino, S-I. & Nishida, H., Jan 1 2018, Promote the Progress of the Pacific-Basin Region through Space Innovation. Misra, A. K., Ming, L. & Morita, Y. (eds.). Univelt Inc., p. 3-7 5 p. (Advances in the Astronautical Sciences; vol. 166).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

parafoils
inflatable structures
Inflatable structures
flight tests
paragliders

Influence of unstable dynamics on orbit determination with x-ray pulsar navigation

Zhou, Y., Bando, M., Hokamoto, S. & Wu, P., Jan 1 2018, Dynamics and Control of Space Systems. Chern, J-S., Luo, Y-Z., Chen, X-Q. & Chen, L. (eds.). Univelt Inc., p. 1827-1843 17 p. (Advances in the Astronautical Sciences; vol. 165).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

orbit determination
navigation
pulsars
Navigation
Orbits

Optimal control of spacecraft attitude motion using Port-Hamiltonian systems

Sakamoto, T., Bando, M. & Hokamoto, S., Jan 1 2018, In : Proceedings of the International Astronautical Congress, IAC. 2018-October

Research output: Contribution to journalConference article

Hamiltonians
optimal control
Spacecraft
spacecraft
Function evaluation

Optimal trajectory design for safety rendezvous based on sparse modeling

Nagashima, S., Bando, M. & Hokamoto, S., Jan 1 2018, In : Proceedings of the International Astronautical Congress, IAC. 2018-October

Research output: Contribution to journalConference article

rendezvous
safety
fuel consumption
trajectory
Trajectories
2 Citations (Scopus)
Multiobjective optimization
Trucks
Constrained optimization
Drones
3 Citations (Scopus)

Station-keeping and formation flying based on nonlinear output regulation theory

Akiyama, Y., Bando, M. & Hokamoto, S., Dec 1 2018, In : Acta Astronautica. 153, p. 289-296 8 p.

Research output: Contribution to journalArticle

Orbits
Satellites
Trajectories
Controllers
Fourier series

Tether cutting maneuver in swing-by trajectory

Yamasaki, T., Bando, M. & Hokamoto, S., Jan 2018, In : Acta Astronautica. 142, p. 212-220 9 p.

Research output: Contribution to journalArticle

Tetherlines
Trajectories
Propellants
Spacecraft
Gravitation

Vertical landing of a fixed-wing UAV using the flat spin

Higashino, S-I. & Nakama, K., Jan 1 2018, 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. International Council of the Aeronautical Sciences, (31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fixed wings
Unmanned aerial vehicles (UAV)
Landing
Propellers
2017

Aerosol Measurements in Antarctica Using “Kite Plane” in January 2017

Hayashi, M., HIrasawa, N., Nakata, K. & Higashino, S-I., May 2017.

Research output: Contribution to conferencePaper

Arrival time assignment by dynamic programming optimization

Matsuda, H., Harada, A., Kozuka, T., Miyazawa, Y. & Wickramasinghe, N. K., Jan 1 2017, Air Traffic Management and Systems II - Selected Papers of the 4th ENRI International Workshop, 2015. Ozeki, S. (ed.). Springer Verlag, p. 185-204 20 p. (Lecture Notes in Electrical Engineering; vol. 420).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Dynamic programming
Trajectories
Airports
Air
Aircraft
19 Citations (Scopus)

Chattering Attenuation Sliding Mode Approach for Nonlinear Systems

Nemati, H., Bando, M. & Hokamoto, S., Jul 2017, In : Asian Journal of Control. 19, 4, p. 1519-1531 13 p.

Research output: Contribution to journalArticle

Sliding mode control
Nonlinear systems
Switching functions
Nonlinear dynamical systems
Derivatives
1 Citation (Scopus)

Considerations on design parameters for attitude control of spacecraft using port-controlled Hamiltonian systems

Sakamoto, T., Akiyama, Y., Bando, M. & Hokamoto, S., Nov 10 2017, 2017 56th Annual Conference of the Society of Instrument and Control Engineers of Japan, SICE 2017. Institute of Electrical and Electronics Engineers Inc., Vol. 2017-November. p. 464-469 6 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hamiltonians
attitude control
Attitude Control
Attitude control
Parameter Design

Formation flying along elliptical orbit using attractive sets of optimal control

Yamane, M., Bando, M. & Hokamoto, S., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 7186-7194 9 p. (Proceedings of the International Astronautical Congress, IAC; vol. 11).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

elliptical orbits
formation flying
optimal control
Orbits
costs

Optic flow-based navigation system for planetary rovers

Kobayashi, N., Bando, M. & Hokamoto, S., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 2839-2847 9 p. (Proceedings of the International Astronautical Congress, IAC; vol. 5).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Navigation systems
navigation
Optics
optics
airborne/spaceborne computers
5 Citations (Scopus)

Orbital plane constraint applicable for in-situ measurement of sub-millimeter-size debris

Furumoto, M., Fujita, K., Hanada, T., Matsumoto, H. & Kitazawa, Y., Mar 15 2017, In : Advances in Space Research. 59, 6, p. 1599-1606 8 p.

Research output: Contribution to journalArticle

in situ measurement
debris
Debris
collision
orbitals

Quantitative analysis of conflict between aircraft by using radar track data

Kozuka, T. & Miyazawa, Y., Jan 1 2017, Air Traffic Management and Systems II - Selected Papers of the 4th ENRI International Workshop, 2015. Ozeki, S. (ed.). Springer Verlag, p. 159-170 12 p. (Lecture Notes in Electrical Engineering; vol. 420).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Radar
Aircraft
Air
Chemical analysis
Controllers

Quaternion based attitude stabilization in the circular restricted three-body problem

Akiyama, Y., Bando, M. & Hokamoto, S., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 750-762 13 p. (Proceedings of the International Astronautical Congress, IAC; vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

quaternions
three body problem
stabilization
Orbits
Stabilization

Simultaneous detection of multiple debris via a cascade of numerical evaluations and a voting scheme for lines in an image sequence

Fujita, K., Ichimura, N. & Hanada, T., Apr 1 2017, In : Acta Astronautica. 133, p. 416-422 7 p.

Research output: Contribution to journalArticle

Debris
Trajectories
Space debris
Orbits
Earth (planet)

Trajectory design to triangular libration points based on resonant orbits

Yamaguchi, N., Bando, M. & Hokamoto, S., Jan 1 2017, 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, p. 7507-7518 12 p. (Proceedings of the International Astronautical Congress, IAC; vol. 11).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

libration
Orbits
trajectory
Trajectories
trajectories
2016

Aerosol Observation and Sample-Return Using a Balloon-Assisted UAV and Results in Antarctica

Higashino, S-I., Hayashi, M., Nagasaki, S., Okada, T. & Ozuka, K., May 2016.

Research output: Contribution to conferencePaper

6 Citations (Scopus)

An orbit determination from debris impacts on measurement satellites

Fujita, K., Tasaki, M., Furumoto, M. & Hanada, T., Jan 15 2016, In : Advances in Space Research. 57, 2, p. 620-626 7 p.

Research output: Contribution to journalArticle

orbit determination
debris
Debris
Orbits
Satellites
1 Citation (Scopus)
planning method
trajectory planning
pilotless aircraft
Unmanned aerial vehicles (UAV)
Motion planning

Aspiration-Point-Based Multiple Objective Path Planning Method for an Unmanned Aerial Vehicle

Omagari, H. & Higashino, S-I., Oct 2016.

Research output: Contribution to conferencePaper

Space debris
space debris
debris
Debris
remediation
3 Citations (Scopus)

Effects of aircraft mass and weather data errors on trajectory optimization and benefits estimation

Wickramasinghe, N. K., Brown, M. A., Miyamoto, Y. & Miyazawa, Y., Jan 1 2016, AIAA Modeling and Simulation Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Modeling and Simulation Technologies Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Trajectory Optimization
Weather
Aircraft
Trajectories
Fuel consumption
2 Citations (Scopus)

Efficient control of arrival time at a congested airport's terminal area

Higuchi, Y., Kitazume, N., Kozuka, T., Tamura, K., Miyazawa, Y. & Brown, M., Jan 1 2016, 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016. International Council of the Aeronautical Sciences, (30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airports
Robust control
Simulators
Experiments
Time of arrival
2 Citations (Scopus)
attitude control
Attitude control
Position control
trajectory
Trajectories

Monitoring the health of geosynchronous spacecraft using photometric observations

Enomoto, T., Hanada, T., Fujita, K. & Kitazawa, Y., Jan 1 2016, In : Proceedings of the International Astronautical Congress, IAC.

Research output: Contribution to journalConference article

health
Spacecraft
space debris
spacecraft
Space debris
1 Citation (Scopus)

On the possibility of using small asteroids for deflecting near-Earth asteroids

Akiyama, Y., Bando, M. & Hokamoto, S., Apr 15 2016, In : Advances in Space Research. 57, 8, p. 1820-1831 12 p.

Research output: Contribution to journalArticle

Asteroids
asteroids
asteroid
Earth (planet)
collision
three body problem
Orbits
orbits
Trajectories
trajectory

Powered swing-by using tether cutting

Yamasaki, T., Bando, M. & Hokamoto, S., Jan 1 2016, In : Proceedings of the International Astronautical Congress, IAC.

Research output: Contribution to journalConference article

tethered satellites
Satellites
maneuvers
Tetherlines
orbits

Satellite formation-keeping about libration points in the presence of system uncertainties

Bando, M., Nemati, H. & Hokamoto, S., Jan 1 2016, Astrodynamics 2015. Turner, J. D., Wawrzyniak, G. G., Cerven, W. T. & Majji, M. (eds.). Univelt Inc., p. 785-804 20 p. (Advances in the Astronautical Sciences; vol. 156).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

libration
sliding
Orbits
Satellites
orbits
2015

A Balloon-Assisted Gliding UAV for Stratospheric Aerosol Observation Using Two-Stage Separation Method in Antarctica

Higashino, S-I., Hayashi, M., Nagasaki, S., Okada, T. & Ozuka, K., Nov 2015.

Research output: Contribution to conferencePaper

3 Citations (Scopus)

Classifying terrain properties for planetary exploration rovers based on a combined distance measure with dynamic texture model

Fujita, K. & Ichimura, N., Aug 1 2015, In : Robotics and Autonomous Systems. 70, p. 156-165 10 p.

Research output: Contribution to journalArticle

Distance Measure
Texture
Textures
Image Sequence
Soil
7 Citations (Scopus)

Correlation between flight time and fuel consumption in airliner flight plan with trajectory optimization

Wickramasinghe, N. K., Brown, M., Fukushima, S., Fukuda, Y., Harada, A. & Miyazawa, Y., Jan 1 2015, AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015. American Institute of Aeronautics and Astronautics Inc., (AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fuel consumption
Trajectories
Aircraft
Costs
Air traffic control

Design of sliding mode controllers for formation flying along unstable periodic orbits in CR3BP

Nemati, H., Bando, M. & Hokamoto, S., 2015, 66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future. International Astronautical Federation, IAF, Vol. 8. p. 5866-5879 14 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

formation flying
sliding
controllers
Orbits
orbits
2 Citations (Scopus)

Dynamic programming trajectory optimization by piecewise linear approximation

Harada, A., Matsuda, H. & Miyazawa, Y., 2015, AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Dynamic programming
Trajectories
Numerical methods
Aircraft
Hardware
11 Citations (Scopus)

Potential benefits of arrival time assignment: Dynamic programming trajectory optimization applied to the Tokyo international airport

Miyazawa, Y., Matsuda, H., Shigetomi, S., Harada, A., Kozuka, T., Wickramasinghe, N. K., Brown, M. & Fukuda, Y., Jan 1 2015.

Research output: Contribution to conferencePaper

arrival time
airport
Dynamic programming
Airports
flight