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Thomas E. Carter
Institution:
Eastern Connecticut State University
Observed institutions:
Worcester Polytechnic Institute,
Eastern Connecticut State University
OpenAlex ID:
A5025392132
State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
1998
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
322
New form for the optimal rendezvous equations near a Keplerian orbit
1990
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
145
Necessary and Sufficient Conditions for Optimal Impulsive Rendezvous with Linear Equations of Motion
2000
·
Thomas E. Carter
·
Dynamics and Control
·
75
Optimal power-limited rendezvous with upper and lower bounds on thrust
1996
·
Thomas E. Carter
, Cyrus J. Pardis
·
Journal of Guidance Control and Dynamics
·
69
Quadratic-Based Computation of Four-Impulse Optimal Rendezvous near Circular Orbit
2000
·
Thomas E. Carter
, Sergio A. Alvarez
·
Journal of Guidance Control and Dynamics
·
53
Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbit
1984
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
47
Optimal power-limited rendezvous with thrust saturation
1995
·
Cyrus J. Pardis
, Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
37
Optimal power-limited rendezvous for linearized equations of motion
1994
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
32
Effects of propellant mass loss on fuel-optimal rendezvous near Keplerian orbit
1989
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
·
14
Closed-form solution of an idealized, optimal, highly eccentric hyperbolic rendezvous problem
1996
·
Thomas E. Carter
·
Dynamics and Control
·
7
Optimal Planar Impulsive Transfer Using Transformed Variables
2018
·
Thomas E. Carter
, Mayer Humi
·
AAS/AIAA Space Flight Mechanics Meeting
·
1
Optimal Power-Limited Rendezvous for Linearized Equations of Motion
1993
·
Thomas E. Carter
·
STIA
·
1
A New Approach to Optimal Impulsive Transfer Near Circular Orbit
2014
·
Thomas E. Carter
, Mayer Humi
·
AIAA/AAS Astrodynamics Specialist Conference and Exhibit
Optimal trajectories based on linear equations
1990
·
Thomas E. Carter
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
Errata: New Form for the Optimal Rendezvous Equations Near a Keplerian Orbit
1990
·
Thomas E. Carter
·
Journal of Guidance Control and Dynamics
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Works count:
15
Citation count:
803
H-index:
9
I10-index:
9
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