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Research Output 2004 2019

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

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

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

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
2017
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

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

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

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

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

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

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

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
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

Orbital maintenance for observation mission of peanut-shaped asteroid

Bando, M., Osuka, K., Fujii, T. & Yamakawa, H., Jan 1 2011, SICE 2011 - SICE Annual Conference 2011, Final Program and Abstracts. Society of Instrument and Control Engineers (SICE), p. 1813-1816 4 p. 6060260. (Proceedings of the SICE Annual Conference).

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

Asteroids
Motion control
Inverse problems
Spacecraft
Gravitation
2010

Active formation along an eccentric orbit

Bando, M. & Ichikawa, A., Jan 1 2010, 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1 ed. IFAC Secretariat, p. 362-367 6 p. (IFAC Proceedings Volumes (IFAC-PapersOnline); vol. 18, no. PART 1).

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

Orbits
Controllers
Feedback
Spacecraft

Application of global solution of Hamilton-Jacobi equations to optimal low-thrust multiple rendezvous problem

Bando, M. & Yamakawa, H., Dec 1 2010, 61st International Astronautical Congress 2010, IAC 2010. p. 9611-9618 8 p. (61st International Astronautical Congress 2010, IAC 2010; vol. 12).

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

low thrust
Hamilton-Jacobi equation
rendezvous
thrust
flyby missions

Atitude dynamics of a pendulum-shaped charged satellite

Yamakawa, H., Hachiyama, S. & Bando, M., 2010, 61st International Astronautical Congress 2010, IAC 2010. Vol. 4. p. 3377-3388 12 p.

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

pendulums
Pendulums
Lorentz force
Satellites
satellite attitude control
1 Citation (Scopus)

Formation flying along a circular orbit with pulse control

Bando, M. & Ichikawa, A., Dec 1 2010, AIAA/AAS Astrodynamics Specialist Conference 2010. (AIAA/AAS Astrodynamics Specialist Conference 2010).

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

Feedback control
Orbits
Acceleration control
Controllability
Feedback

From elliptic restricted three-body problem to Tschauner-Hempel equations: A control strategy based on circular problems

Bando, M. & Ichikawa, A., Dec 1 2010, Astrodynamics 2009 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. p. 301-313 13 p. (Advances in the Astronautical Sciences; vol. 135).

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

three body problem
natural satellites
Moon
halos
Orbits

Gravity-coulomb force combined three-body problem

Yamakawa, H. & Bando, M., Jan 1 2010, 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings. PART 1 ed. IFAC Secretariat, p. 350-355 6 p. (IFAC Proceedings Volumes (IFAC-PapersOnline); vol. 18, no. PART 1).

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

Electrostatics
Gravitation
1 Citation (Scopus)

Low-thrust trajectory optimization using second-order generating functions

Bando, M. & Yamakawa, H., Jan 1 2010, Proceedings of SICE Annual Conference 2010, SICE 2010 - Final Program and Papers. Society of Instrument and Control Engineers (SICE), p. 804-810 7 p. 5603000. (Proceedings of the SICE Annual Conference).

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

Trajectories
Space rendezvous
Hamiltonians
Disturbance rejection
Boundary value problems

Near-Earth asteroid survey mission concept using solar sailing technology

Bando, M. & Yamakawa, H., Dec 1 2010, Applications of Space Technology for Humanity - Advances in the Astronautical Sciences: Proceedings of the 12th International Conference of Pacific-Basin Societies, ISCOPS. p. 257-269 13 p. (Advances in the Astronautical Sciences; vol. 138).

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

Asteroids
ice ridge
asteroids
asteroid
Spacecraft
1 Citation (Scopus)

Solution to lambert's problem using generalized canonical transformations

Bando, M. & Yamakawa, H., Dec 1 2010, Spaceflight Mechanics 2010 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Space Flight Mechanics Meeting. p. 587-603 17 p. (Advances in the Astronautical Sciences; vol. 136).

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

optimal control
flyby missions
astrodynamics
Space flight
Control theory
13 Citations (Scopus)

Spacecraft relative dynamics under the influence of geomagnetic lorentz force

Yamakawa, H., Bando, M., Yano, K. & Tsujii, S., Dec 1 2010, AIAA/AAS Astrodynamics Specialist Conference 2010. (AIAA/AAS Astrodynamics Specialist Conference 2010).

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

Lorentz force
Spacecraft
Orbits
Electromagnetic propulsion
Earth (planet)
2009
11 Citations (Scopus)

A new optimal orbit control for two-point boundary-value problem using generating functions

Bando, M. & Yamakawa, H., Dec 1 2009, Spaceflight Mechanics 2009 - Advances in the Astronautical Sciences: Proceedings of the 19th AAS/AIAA Space Flight Mechanics Meeting. p. 245-260 16 p. (Advances in the Astronautical Sciences; vol. 134).

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

optimal control
boundary value problems
Boundary value problems
Orbits
orbits

Satellite formation with restricted control interval

Ichikawa, A. & Bando, M., Dec 11 2009, Proceedings of 2009 7th Asian Control Conference, ASCC 2009. p. 69-74 6 p. 5276277. (Proceedings of 2009 7th Asian Control Conference, ASCC 2009).

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

Orbits
Satellites
Feedback control
Riccati equations
Controllability
2007
3 Citations (Scopus)

Adaptive output regulation of nonlinear systems described by multiple linear models

Bando, M. & Ichikawa, A., Dec 1 2007, 9th IFAC Workshop "Adaptation and Learning in Control and Signal Processing", ALCOSP'2007 - Final Program and Abstracts. PART 1 ed. p. 269-274 6 p. (IFAC Proceedings Volumes (IFAC-PapersOnline); vol. 9, no. PART 1).

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

Nonlinear systems
Controllers
2006
3 Citations (Scopus)

Adaptive output regulation for linear systems

Bando, M. & Ichikawa, A., 2006, 2006 SICE-ICASE International Joint Conference. p. 3217-3222 6 p. 4108312

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

Linear systems
Controllers
State feedback