Robust deflection strategies of Near Earth asteroids under uncertainties

Mai Bando, Yuki Akiyama, Shinji Hokamoto

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

Abstract

In this paper, an approach to optimize deflection mission of Near Earth asteroids under uncertainty is proposed based on control theoretical framework. By using the nonlinear mapping from initial deviation to the final deviation, the performance index J which is expressed as a function of the distance of the Earth in the Earth's closest approach time is minimized for the worst case initial condition. We also formulate the robust orbital transfer problem of kinetic impactor spacecraft where the initial state estimation error exists.

Original languageEnglish
Title of host publicationAdvances In The Astronautical Sciences
EditorsDonald L. Mackison, Ossama Abdelkhalik, Roby S. Wilson, Renato Zanetti
PublisherUnivelt Inc.
Pages1165-1181
Number of pages17
ISBN (Electronic)9780877036111
Publication statusPublished - Jan 1 2014
Event24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States
Duration: Jan 26 2014Jan 30 2014

Publication series

NameAdvances in the Astronautical Sciences
Volume152
ISSN (Print)0065-3438

Other

Other24th AAS/AIAA Space Flight Mechanics Meeting, 2014
CountryUnited States
CityMexico
Period1/26/141/30/14

Fingerprint

Asteroids
asteroids
deflection
asteroid
Earth (planet)
deviation
transfer orbits
Orbital transfer
state estimation
impactors
State estimation
Spacecraft
spacecraft
kinetics
Kinetics
Uncertainty

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Bando, M., Akiyama, Y., & Hokamoto, S. (2014). Robust deflection strategies of Near Earth asteroids under uncertainties. In D. L. Mackison, O. Abdelkhalik, R. S. Wilson, & R. Zanetti (Eds.), Advances In The Astronautical Sciences (pp. 1165-1181). (Advances in the Astronautical Sciences; Vol. 152). Univelt Inc..

Robust deflection strategies of Near Earth asteroids under uncertainties. / Bando, Mai; Akiyama, Yuki; Hokamoto, Shinji.

Advances In The Astronautical Sciences. ed. / Donald L. Mackison; Ossama Abdelkhalik; Roby S. Wilson; Renato Zanetti. Univelt Inc., 2014. p. 1165-1181 (Advances in the Astronautical Sciences; Vol. 152).

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

Bando, M, Akiyama, Y & Hokamoto, S 2014, Robust deflection strategies of Near Earth asteroids under uncertainties. in DL Mackison, O Abdelkhalik, RS Wilson & R Zanetti (eds), Advances In The Astronautical Sciences. Advances in the Astronautical Sciences, vol. 152, Univelt Inc., pp. 1165-1181, 24th AAS/AIAA Space Flight Mechanics Meeting, 2014, Mexico, United States, 1/26/14.
Bando M, Akiyama Y, Hokamoto S. Robust deflection strategies of Near Earth asteroids under uncertainties. In Mackison DL, Abdelkhalik O, Wilson RS, Zanetti R, editors, Advances In The Astronautical Sciences. Univelt Inc. 2014. p. 1165-1181. (Advances in the Astronautical Sciences).
Bando, Mai ; Akiyama, Yuki ; Hokamoto, Shinji. / Robust deflection strategies of Near Earth asteroids under uncertainties. Advances In The Astronautical Sciences. editor / Donald L. Mackison ; Ossama Abdelkhalik ; Roby S. Wilson ; Renato Zanetti. Univelt Inc., 2014. pp. 1165-1181 (Advances in the Astronautical Sciences).
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