Unconstrained direct optimization of spacecraft trajectories using many embedded Lambert problems
type: Item
instance of: scholarly article
title: Unconstrained direct optimization of spacecraft trajectories using many embedded Lambert problems
zbMATH Open document ID: 1483.49007
author: David Ottesen
author: Ryan P. Russell
published in: Journal of Optimization Theory and Applications
publication date: 2021-12-01T00:00:00Z
Mathematics Subject Classification ID: 49J10
zbMATH DE Number: 7436671
zbMATH Keywords: spacecraft
zbMATH Keywords: trajectory
zbMATH Keywords: unconstrained direct optimization
zbMATH Keywords: Lambert
zbMATH Keywords: embedded boundary value problem
zbMATH Keywords: trajectory optimization
describes a project that uses: SNOPT
MaRDI profile type: Publication
full work available at URL: s10957-021-01884-1
OpenAlex ID: W3182050111
cites work: Q4868576
cites work: Logarithmic Spiral: An Ideal Trajectory for the Interplanetary Vehicle with Engines of Low Sustained Thrust
cites work: A survey of efficient computational methods for manipulator inverse dynamics
cites work: Q4954189
cites work: Survey of Numerical Methods for Trajectory Optimization
cites work: Trajectory optimization on a parallel processor
cites work: Geometric orbital transfer using averaging techniques
cites work: The Convergence of a Class of Double-rank Minimization Algorithms 1. General Considerations
cites work: Representations of quasi-Newton matrices and their use in limited memory methods
cites work: A survey of methods available for the numerical optimization of continuous dynamic systems
cites work: Application of high order expansions of two-point boundary value problems to astrodynamics
cites work: Optimal transfers between unstable periodic orbits using invariant manifolds
cites work: A new approach to variable metric algorithms
cites work: Function minimization by conjugate gradients
cites work: SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization
cites work: Lagrange multipliers and the state transition matrix for coasting arcs.
cites work: A Family of Variable-Metric Methods Derived by Variational Means
cites work: A procedure for the solution of Lambert's orbital boundary-value problem
cites work: A New Conjugate Gradient Method with Guaranteed Descent and an Efficient Line Search
cites work: Q5479892
cites work: Transfers between libration-point orbits in the elliptic restricted problem
cites work: Revisiting Lambert's problem
cites work: Search space pruning and global optimisation of multiple gravity assist spacecraft trajectories
cites work: Primer vector theory applied to the linear relative-motion equations
cites work: An efficient method for calculating optimal free-space n-impulse trajectories.
cites work: A hybrid differential dynamic programming algorithm for constrained optimal control problems. I: Theory
cites work: A hybrid differential dynamic programming algorithm for constrained optimal control problems. II: Application
cites work: Basic Linear Algebra Subprograms for Fortran Usage
cites work: Primer vector on fixed-time impulsive trajectories.
cites work: Q3875412
cites work: The theory of connections: connecting points
cites work: Q5563083
cites work: On the solution to every Lambert problem
cites work: Conditioning of Quasi-Newton Methods for Function Minimization
cites work: Universal Keplerian state transition matrix
cites work: Averaging Techniques and Their Application to Orbit Determination Systems
DOI: 10.1007/S10957-021-01884-1
description: scientific article; zbMATH DE number 7436671