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Research Output 2004 2019

  • 213 Citations
  • 10 h-Index
  • 39 Conference contribution
  • 25 Article
  • 4 Conference article
  • 2 Paper
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

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

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
1 Citation (Scopus)

Nonlinear attractive and reachable sets under optimal control in three-body problem

Bando, M. & Scheeres, D. J., Jan 1 2018, In : Journal of Guidance, Control, and Dynamics. 41, 8, p. 1766-1775 10 p.

Research output: Contribution to journalArticle

Three-body Problem
Reachable Set
three body problem
optimal control
Optimal Control

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)

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 1 2018, In : Acta Astronautica. 142, p. 212-220 9 p.

Research output: Contribution to journalArticle

Tetherlines
Trajectories
Propellants
Spacecraft
Gravitation
2017
18 Citations (Scopus)

Chattering Attenuation Sliding Mode Approach for Nonlinear Systems

Nemati, H., Bando, M. & Hokamoto, S., 2017, (Accepted/In press) In : Asian Journal of Control.

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

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

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

Attractive set of optimal feedback control for the hill three-body problem

Bando, M. & Scheeres, D. J., 2016, Spaceflight Mechanics 2016. Univelt Inc., Vol. 158. p. 471-488 18 p.

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

three body problem
optimal control
feedback control
Feedback control
spacecraft trajectories
4 Citations (Scopus)

Attractive sets to unstable orbits using optimal feedback control

Bando, M. & Scheeres, D. J., Jan 1 2016, In : Journal of Guidance, Control, and Dynamics. 39, 12, p. 2725-2739 15 p.

Research output: Contribution to journalArticle

Optimal Feedback Control
feedback control
Feedback control
Orbits
Orbit

Nonlinear attractive sets under optimal feedback control in the hill three-body problem

Bando, M. & Scheeres, D. J., 2016, AIAA/AAS Astrodynamics Specialist Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA

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

three body problem
feedback control
Partial differential equations
Feedback control
Nonlinear systems
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., 2016, In : Proceedings of the International Astronautical Congress, IAC.

Research output: Contribution to journalArticle

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

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
7 Citations (Scopus)

Formation flying along halo orbit of circular-restricted three-Body problem

Bando, M. & Ichikawa, A., Jan 1 2015, In : Journal of Guidance, Control, and Dynamics. 38, 1, p. 123-129 7 p.

Research output: Contribution to journalArticle

Formation Flying
Restricted Three-body Problem
formation flying
three body problem
halos

Optimal selection of impulse times for formation flying

Bando, M. & Ichikawa, A., 2015, 2nd IAA Conference on Dynamics and Control of Space Systems, 2014. Univelt Inc., Vol. 153. p. 861-872 12 p.

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

formation flying
impulses
Orbits
orbits
fuel consumption
2014

Estimation of mean orbital elements with unknown low-thrust acceleration

Bando, M., Date, N. & Hokamoto, S., 2014, 65th International Astronautical Congress 2014, IAC 2014: Our World Needs Space. International Astronautical Federation, IAF, Vol. 7. p. 4645-4655 11 p.

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

low thrust
orbital elements
Spacecraft
thrust
low thrust propulsion

Formation flying along an elliptic orbit by pulse control

Bando, M. & Ichikawa, A., Jan 1 2014, Astrodynamics 2013 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. Univelt Inc., p. 1433-1446 14 p. (Advances in the Astronautical Sciences; vol. 150).

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

formation flying
Orbits
orbits
pulses
linear quadratic regulator

Robust deflection strategies of Near Earth asteroids under uncertainties

Bando, M., Akiyama, Y. & Hokamoto, S., 2014, Advances In The Astronautical Sciences. Univelt Inc., Vol. 152. p. 1165-1181 17 p.

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

Asteroids
asteroids
deflection
asteroid
Earth (planet)

Wide-field-integration of optic flow for realistic estimation system for space probes

Hokamoto, S., Oishi, M., Kobayashi, N. & Bando, M., Jan 1 2014, 65th International Astronautical Congress 2014, IAC 2014: Our World Needs Space. International Astronautical Federation, IAF, p. 5151-5159 9 p. (Proceedings of the International Astronautical Congress, IAC; vol. 7).

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

Space probes
space probes
photoreceptors
Optics
field of view
2013

Active formation along a circular orbit by pulse control

Bando, M. & Ichikawa, A., Jan 1 2013, p. 2197-2203. 7 p.

Research output: Contribution to conferencePaper

Orbits
Linear systems
Differential equations
Satellites
11 Citations (Scopus)

Engineering notes active formation flying along an elliptic orbit

Bando, M. & Ichikawa, A., Jan 1 2013, In : Journal of Guidance, Control, and Dynamics. 36, 1, p. 324-332 9 p.

Research output: Contribution to journalArticle

Formation Flying
formation flying
Orbits
Orbit
engineering

Flying near the libration points by impulse control

Bando, M. & Ichikawa, A., 2013, In : Unknown Journal. 148, p. 3045-3057 13 p.

Research output: Contribution to journalArticle

libration
impulses
Orbits
flight
orbits
6 Citations (Scopus)

In-plane motion control of Hill-Clohessy-Wiltshire equations by single input

Bando, M. & Ichikawa, A., Sep 1 2013, In : Journal of Guidance, Control, and Dynamics. 36, 5, p. 1512-1521 10 p.

Research output: Contribution to journalArticle

Motion Control
Motion control
controllers
Controller
Controllers

Proposal of buckling-type-driving-unit for rover on small gravity asteroid

Osuka, K., Mochiyama, H., Tadakuma, K., Bando, M. & Ohgata, K., 2013, SICE 2013: International Conference on Instrumentation, Control, Information Technology and System Integration - SICE Annual Conference 2013, Conference Proceedings. p. 642-643 2 p.

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

Asteroids
Buckling
Gravitation
Rockets
28 Citations (Scopus)

Spacecraft formation flying dynamics and control using the geomagnetic lorentz force

Tsujii, S., Bando, M. & Yamakawa, H., Jan 1 2013, In : Journal of Guidance, Control, and Dynamics. 36, 1, p. 136-148 13 p.

Research output: Contribution to journalArticle

Formation Flying
formation flying
Lorentz force
Quadratic programming
Spacecraft

Trajectory design of destiny mission

Bando, M., Nakamiya, M., Kawakatsu, Y., Hirose, C. & Yamamoto, T., Apr 24 2013, Space for Our Future - Advances in the Astronautical Sciences: Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012. Vol. 146. p. 321-322 2 p.

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

trajectory
Trajectories
trajectories
trajectory optimization
low thrust
2012
21 Citations (Scopus)

Attitude dynamics of a pendulum-shaped charged satellite

Yamakawa, H., Hachiyama, S. & Bando, M., Jan 1 2012, In : Acta Astronautica. 70, p. 77-84 8 p.

Research output: Contribution to journalArticle

Pendulums
Satellites
Lorentz force
Attitude control
Magnetic fields

Formation flying along a circular orbit with control constraints

Bando, M. & Ichikawa, A., Dec 1 2012, ASTRODYNAMICS 2011 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. p. 1375-1388 14 p. (Advances in the Astronautical Sciences; vol. 142).

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

formation flying
circular orbits
norms
Orbits
orbits
11 Citations (Scopus)

Graphical generation of periodic orbits of tschauner-hempel equations

Bando, M. & Ichikawa, A., May 1 2012, In : Journal of Guidance, Control, and Dynamics. 35, 3, p. 1002-1007 6 p.

Research output: Contribution to journalArticle

Periodic Orbits
Orbits
orbits
Orbit
Eccentricity

On the optimality of plug-in optimal control systems

Fujii, T., Osuka, K. & Bando, M., 2012, International MultiConference of Engineers and Computer Scientists, IMECS 2012. Newswood Limited, Vol. 2196. p. 952-955 4 p.

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

Optimal control systems
Control systems
Feedback control
Poles
Controllers
2011
2 Citations (Scopus)

Near-Earth asteroid flyby survey mission using solar sailing technology

Bando, M. & Yamakawa, H., Jan 1 2011, In : Journal of the Astronautical Sciences. 58, 4, p. 569-581 13 p.

Research output: Contribution to journalArticle

Asteroids
ice ridge
asteroids
asteroid
Spacecraft
1 Citation (Scopus)

On optimality and integrity of plug-in optimal control

Osuka, K., Fujii, T. & Bando, M., 2011, SICE 2011 - SICE Annual Conference 2011, Final Program and Abstracts. p. 2249-2250 2 p. 6060347

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

Control systems
12 Citations (Scopus)

Optimal pulse strategies for relative orbit transfer along a circular orbit

Jifuku, R., Ichikawa, A. & Bando, M., Sep 1 2011, In : Journal of Guidance, Control, and Dynamics. 34, 5, p. 1329-1341 13 p.

Research output: Contribution to journalArticle

transfer orbits
Orbital transfer
circular orbits
Orbits
Orbit