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[HTML][HTML] Survey of orbital dynamics and control of space rendezvous
Y Luo, J Zhang, G Tang - Chinese Journal of Aeronautics, 2014 - Elsevier
Rendezvous orbital dynamics and control (RODC) is a key technology for operating space
rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the …
rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the …
On the solution to every Lambert problem
RP Russell - Celestial Mechanics and Dynamical Astronomy, 2019 - Springer
Lambert's problem is the two-point boundary value problem for Keplerian dynamics. The
parameter and solution space is surveyed for both the zero-and multiple-revolution …
parameter and solution space is surveyed for both the zero-and multiple-revolution …
Complete Lambert solver including second-order sensitivities
RP Russell - Journal of Guidance, Control, and Dynamics, 2022 - arc.aiaa.org
The complete parameter space for Lambert's problem includes all possible geometries, flight
times, and revolutions. An earlier work exploited a rectangular form of this parameter space …
times, and revolutions. An earlier work exploited a rectangular form of this parameter space …
Optimal multi-objective linearized impulsive rendezvous
The multi-objective optimization of linearized impulsive rendezvous is investigated in this
paper and this optimization includes the minimum characteristic velocity, the minimum time …
paper and this optimization includes the minimum characteristic velocity, the minimum time …
Stability analysis of linear impulsive delay dynamical systems via looped-functionals
This article investigates the asymptotic stability of impulsive delay dynamical systems (IDDS)
by using the Lyapunov–Krasovskii method and looped-functionals. The proposed conditions …
by using the Lyapunov–Krasovskii method and looped-functionals. The proposed conditions …
Terminal-velocity-based Lambert algorithm
G Zhang - Journal of Guidance, Control, and Dynamics, 2020 - arc.aiaa.org
This paper provides an alternative Lambert solution based on the terminal velocity vector.
The chordal terminal velocity component is selected as the independent variable since it is …
The chordal terminal velocity component is selected as the independent variable since it is …
Solution of the Probabilistic Lambert Problem: Connections with Optimal Mass Transport, Schr\" odinger Bridge and Reaction-Diffusion PDEs
The Lambert problem originated in orbital mechanics. It concerns with determining the initial
velocity for a boundary value problem involving the dynamical constraint due to gravitational …
velocity for a boundary value problem involving the dynamical constraint due to gravitational …
Peer-to-peer refueling for circular satellite constellations
The scheduling problem arising from refueling multiple satellites in a circular constellation is
studied. It is assumed that no fuel is delivered to the constellation from an external source …
studied. It is assumed that no fuel is delivered to the constellation from an external source …
Homotopic perturbed Lambert algorithm for long-duration rendezvous optimization
LAMBERT, s problem has been discussed over the years by many researchers [1–3]. Gauss
[1] first developed an iterative method to solve Lambert, s problem, which is efficient and …
[1] first developed an iterative method to solve Lambert, s problem, which is efficient and …
Optimization of multiple-impulse, multiple-revolution, rendezvous-phasing maneuvers
A new hybrid optimization approach is proposed for the design of a rendezvous-phasing
strategy with combined maneuvers, which is normally considered as a complex multiple …
strategy with combined maneuvers, which is normally considered as a complex multiple …