CONSTANT ATTITUDE THRUST PROGRAM OPTIMIZATION
Optimum thrust programming studies include a comparison of constant and variable attitude thrust programs for an earth-mars rendezvous
THRUST PROGRAMMING↗
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Constant-attitude thrust program optimization.
Optimum thrust programming studies include comparison of constant and variable attitude thrust programs for Earth-Mars rendezvous
TRAJECTORY OPTIMIZATION↗
A preliminary analysis of orbit insertion guidance for the Voyager mission
Guidance laws for propellant efficiency with optimum thrust program and error analysis for Voyager mission orbit insertion
OPTIMUM THRUST PROGRAMMING↗
Optical ascent into orbit - a new look at an old problem.
Optimum thrust programming of ascent trajectory for orbiting space vehicle, using parameter variation method
STEEPEST ASCENT METHOD↗
Interplanetary guidance system requirements study. Volume 2 - Computer program descriptions. Part 9 - Program description for optimum low thrust trajectories
Computer program for optimization of low thrust interplanetary trajectories assuming constant and continuous thrust from given initial and final position, velocity and flight time
Source record↗
Quasilinearization program for determining optimum finite-thrust transfers between inclined orbits
Quasi-linearization program for boundary value problem of minimum fuel orbital transfer
Bender, D. F.↗
A dynamic programing analysis of multiple guidance corrections of a trajectory.
Adaptive guidance correction policy developed from dynamic programming point of view for perturbed trajectory of spacecraft
SPACECRAFT TRAJECTORY↗
Method of characteristic constants and retro- thrust optimality in a gravitational field - necessary and sufficient conditions.
Intermediate thrust sub-arcs analyzed by method of characteristic constants for optimum retrothrust program in inverse-square-law force field
BOUNDARY VALUE↗
An explicit solution for the Lagrange multipliers on the singular subarc of an optimal trajectory
Explicit solution for Lagrange multipliers in optimal thrust programming and steering problem
LAGRANGE MULTIPLIER↗
OPTIMUM INTERPLANETARY RENDEZVOUS WITH POWER-LIMITED VEHICLES
Optimum interplanetary rendezvous with power limited vehicles
SPACE FLIGHT↗
Constants of the motion for optimum thrust trajectories in a central force field
Constants of motion for optimum thrust trajectories in central force field
OPTIMUM THRUST PROGRAMMING↗
Optimum retro-thrust in a gravitational field
Optimal retrothrust in gravitational field
OPTIMUM THRUST PROGRAMMING↗
Constants of the motion for optimum thrust trajectories in a central force field.
Motion constants for optimal thrust trajectories in central force field by iterative procedure
MOTION EQUATION↗
Design of optimized three-dimensional rocket motor nozzles.
Optimization of supersonic portion of three- dimensional flow geometry in rocket motor nozzle for maximum thrust
THREE-DIMENSIONAL FLOW↗
Powered flight trajectory optimization for lunar and interplanetary transfer.
Steepest descent method to compute powered flight trajectory optimization for lunar and interplanetary transfer
TRAJECTORY OPTIMIZATION↗
Orbital transfer by optimum thrust direction and duration
Orbital transfer by optimum thrust direction and duration
ORBITAL TRANSFER↗
A linear theory of optimum low-thrust rendezvous trajectories.
Linear theory of optimum variable thrust rendezvous trajectories with power limit propulsion system
LINEAR EQUATION↗
How many impulses/ques/
Minimum fuel transfer solution of Lawden problem involving finite number of impulse thrusts separated by coasting arcs
OPTIMUM THRUST PROGRAMMING↗