A DISCUSSION OF GUIDANCE POLICIES FOR MULTIPLE-IMPULSE CORRECTION OF THE TRAJECTORY OF A SPACECRAFT
Guidance policies for multiple-impulse correction of spacecraft trajectory
SPACECRAFT TRAJECTORY↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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NONLINEAR GUIDANCE SYSTEM FOR DESCENT TRAJECTORIES
Nonlinear guidance system for descent trajectories
DESCENT TRAJECTORY↗
GUIDANCE CONCEPTS FOR LUNAR LANDING
Interrupted-braking guidance system for soft lunar landings
GUIDANCE (MOTION)↗
APPLICATION OF AN ''ITERATIVE GUIDANCE MODE'' TO A LUNAR LANDING
Optimization of space-vehicle trajectories by use of iterative guidance mode that minimizes midflight recalculation time for new optimum trajectories
SPACECRAFT GUIDANCE↗
USE OF CALCULUS OF VARIATIONS METHODS FOR TRAJECTORY OPTIMIZATION AND ADVANCED GUIDANCE CONCEPTS
Calculus of variation methods used for trajectory optimization and guidance of rocket propelled vehicles
TRAJECTORY CONTROL↗
TRAJECTORY AND GUIDANCE CONSIDERATIONS FOR LUNAR RETURN MISSIONS
Problems involved in meeting trajectory and guidance requirements for the return-to-earth and atmospheric reentry of a lunar spacecraft
SPACECRAFT GUIDANCE↗
An Iterative Guidance Scheme for Ascent to Orbit (Suborbital Start of the Third Stage)
Motion equations - iterative guidance scheme for ascent to orbit
ASCENT TRAJECTORY↗
Space flight and guidance theory- introduc- tion
Nasa research in space flight and guidance theory
NASA PROGRAM↗
Guidance equations for quasi-optimum space maneuvers
Approximate time optimum guidance equations for planetary ascent and descent trajectories at constant thrust flat body two-dimensional case
GUIDANCE↗
Space vehicle guidance-a boundary value formulation. part ii- boundary conditions with parameters
Boundary value formulation of space vehicle guidance problem
GUIDANCE↗
Guidance of unmanned lunar and interplanetary spacecraft
Earth-based guidance of unmanned lunar and interplanetary spacecraft
UNMANNED SPACECRAFT↗
Application of an iterative guidance mode to a lunar landing <anwendung eines iterativen lenkverfahren auf eine mondlandung<.
Iterative guidance mode applied to lunar landing for optimization of trajectories for minimum propellant consumption
ITERATIVE SOLUTION↗
A dynamic programming analysis of multiple guidance corrections of a trajectory /revision no. 1/
Dynamic programming applied to guidance correction for perturbed trajectory of spacecraft
SPACECRAFT TRAJECTORY↗
Guidance applications of linear analysis
Differential equations of motion linearized about nominal calculus of variation solution to determine coefficients of guidance function
VARIATIONAL CALCULUS↗
Simplified technique for aborting a lunar landing mission during powered descent using manual backup guidance
Simplified technique for aborting lunar landing mission during powered descent using manual backup guidance
LUNAR LANDING↗
Guidance of a low l/d vehicle entering the earth's atmosphere at speeds up to 50,000 feet per second
Guidance of low lift-drag ratio vehicle during earth atmosphere reentry
LIFT-DRAG RATIO↗
A boundary value formulation for space vehicle guidance
Boundary value formulation for space vehicle guidance and control
BOUNDARY VALUE PROBLEM↗
An iterctive guidance scheme and its applica- tion to lunar landing
Guidance scheme for vehicle flight from lunar orbit to prescribed point on spherical nonrotating moon
GUIDANCE SYSTEM↗