Primer vector theory is used in analyzing a set of linear, relative-motion equations - the Clohessy-Wiltshire equations - to determine the criteria and necessary conditions for an optimal, N-impulse trajectory. Since the state vector for these equations is defined in terms of a linear system of ordinary differential equations, all fundamental relations defining the solution of the state and costate equations, and the necessary conditions for optimality, can be expressed in terms of elementary functions. The analysis develops the analytical criteria for improving a solution by (1) moving any dependent or independent variable in the initial and/or final orbit, and (2) adding intermediate impulses. If these criteria are violated, the theory es...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
The primer vector theory, firstly proposed by Lawden, defines a set of necessary conditions to chara...
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial vel...
A method developed to compute two-body, optimal, N-impulse trajectories was presented. The necessary...
Trajectory optimisation during the preliminary design phase is crucial for a mission designer to mee...
Method for numerical solutions of nonlinear optimum trajectory problems using approximate analytic m...
This paper examines the primer vector which governs optimal solutions for orbital transfer when the ...
Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust varia...
Over the past years, the commercial interest in returning to the Moon and exploring the deep space h...
The primer vector theory, firstly proposed by Lawden, defines a set of necessary conditions to chara...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
This report presents the formulation of the optimal low- and medium-thrust orbit transfer control pr...
For the case of impulsive thrust trajectories, Lawden’s primer vector theory gives a set of necessar...
International audienceThe problem of fixed-time fuel-optimal trajectories with high-thrust propulsio...
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
The primer vector theory, firstly proposed by Lawden, defines a set of necessary conditions to chara...
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial vel...
A method developed to compute two-body, optimal, N-impulse trajectories was presented. The necessary...
Trajectory optimisation during the preliminary design phase is crucial for a mission designer to mee...
Method for numerical solutions of nonlinear optimum trajectory problems using approximate analytic m...
This paper examines the primer vector which governs optimal solutions for orbital transfer when the ...
Minimum-fuel trajectories in the Clohessy-Wiltshire orbital model are investigated. Low-thrust varia...
Over the past years, the commercial interest in returning to the Moon and exploring the deep space h...
The primer vector theory, firstly proposed by Lawden, defines a set of necessary conditions to chara...
Within the field of trajectory optimisation, Lawden developed the primer vector theory, which define...
This report presents the formulation of the optimal low- and medium-thrust orbit transfer control pr...
For the case of impulsive thrust trajectories, Lawden’s primer vector theory gives a set of necessar...
International audienceThe problem of fixed-time fuel-optimal trajectories with high-thrust propulsio...
Simplified and accurate relative equations of motion for two impulse orbital rendezvou
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
The primer vector theory, firstly proposed by Lawden, defines a set of necessary conditions to chara...
Optimum transfer between two terminal points for minimum initial impulse under arbitrary initial vel...