Bruce A Conway

1982 …2018
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Research Output 1982 2018

Analytic gradient computation for bounded-impulse trajectory models using two-sided shooting

Ellison, D. H., Conway, B. A., Englander, J. A. & Ozimek, M. T., Jul 2018, In : Journal of Guidance, Control, and Dynamics. 41, 7, p. 1449-1462 14 p.

Research output: Contribution to journalArticle

Shooting
Partial derivative
Impulse
impulses
trajectory

Application and analysis of bounded-impulse trajectory models with analytic gradients

Ellison, D. H., Conway, B. A., Englander, J. A. & Ozimek, M. T., Jan 1 2018, In : Journal of Guidance, Control, and Dynamics. 41, 8, p. 1700-1714 15 p.

Research output: Contribution to journalArticle

Impulse
impulses
trajectory
Trajectories
trajectories

Optimal nonlinear feedback with feedforward control of high speed aerospace vehicles using a spatial statistical approach

Chilan, C. M., Conway, B. A., Bialy, B. J. & Stockbridge, S., Jan 1 2018, AAS/AIAA Astrodynamics Specialist Conference, 2018. Singla, P., Weisman, R. M., Marchand, B. G. & Jones, B. A. (eds.). Univelt Inc., p. 997-1016 20 p. (Advances in the Astronautical Sciences; vol. 167).

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

aerospace vehicles
Aerospace vehicles
nonlinear feedback
feedforward control
Nonlinear feedback

Optimal trajectories for hyperbolic rendezvous with earth-mars cycling spacecraft

Pontani, M. & Conway, B. A., Jan 1 2018, In : Journal of Guidance, Control, and Dynamics. 41, 2, p. 360-376 17 p.

Research output: Contribution to journalArticle

rendezvous
Mars
Rendezvous
Optimal Trajectory
Cycling

Asteroid deflection with safe harbors found via numerical optimization

Conway, B. A., Eggl, S. & Hestroffer, D., Jan 1 2017, Spaceflight Mechanics 2017. Sims, J. A., Leve, F. A., McMahon, J. W. & Guo, Y. (eds.). Univelt Inc., p. 565-575 11 p. (Advances in the Astronautical Sciences; vol. 160).

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

Asteroids
harbors
Ports and harbors
asteroids
deflection