LUNAR LANDING AND LONG-RANGE EARTH REENTRY GUIDANCE BY APPLICATION OF PERTURBATION THEORY
Lunar landing & long range earth reentry guidance by single nominal trajectory using perturbation theory
LUNAR LANDING↗
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A SURVEY OF ATMOSPHERE REENTRY GUIDANCE AND CONTROL METHODS
Guidance and control methods for spacecraft atmospheric reentry
CONTROL↗
CONTROL AND GUIDANCE OF ELECTRICALLY PROPELLED SPACECRAFT
Flight trajectory, control, guidance and equipment limitations of nuclear-electric spacecraft
SPACECRAFT DESIGN↗
THE USE OF MAN IN BOOSTER GUIDANCE AND CONTROL
Flight simulation of piloted booster systems to determine control and guidance concepts, pilot simulator performance, and pilot trajectory control
FLIGHT SIMULATION↗
SURVEY OF ATMOSPHERE RE-ENTRY GUIDANCE AND CONTROL METHODS
Guidance and control methods for spacecraft atmospheric reentry
CONTROL↗
On studies in the field of space flight and guidance theory progress report no. 4 <20 dec. 1962 - 18 jul. 1963<
Trajectories, orbital calculations, and adaptive guidance
ORBIT CALCULATION↗
An optimal guidance approximation theory
Optimal guidance approximations using perturbation theory
OPTIMAL CONTROL↗
Future guidance and leadership in science and technology
Scientific research and future guidance and leadership in science and technology
LEADERSHIP↗
Fixed-base-simulator study of ability of pilots to perform soft lunar landings by using a simplified guidance technique
Fixed base simulator study of pilot ability to perform soft lunar landing with simplified guidance technique
LUNAR LANDING↗
Simple Guidance for Deep-Space Booster Vehicles
A relatively simple injection-guidance system used in conjunction with post-injection midcourse correction will be adequate for lunar and interplanetary missions.
Pfeiffer, C.↗
Two-body linear guidance matrices
Analytical expressions for two-body linear guidance matrices in velocity dependent coordinate system for variant motion equation solutions
COORDINATE SYSTEM↗
Manual abort guidance from the midcourse region of a lunar mission
Manual abort guidance from midcourse region of lunar mission
ABORT TRAJECTORY↗
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
OPTIMAL CONTROL↗
Optimum guidance for a low thrust interplanetary vehicle.
Optimum guidance in two dimensions of constant acceleration low-thrust vehicle spiraling away from and in toward planet
OPTIMAL CONTROL↗
An ensemble averaging approach to optimal guidance polynomial approximations.
Synthesis parametry of ensemble-averaged second- order polynomial approximation to performance index of optimal guidance linear feedback control system
APPROXIMATION METHOD↗
Star/horizon simulator used to test space guidance system
Star/horizon simulator is used for alignment and optical plus photoelectric tests of the sextant for the Apollo guidance and navigation system optical unit assembly. The unit is basically a refractive collimator with a two inch objective lens system and a twenty-four inch focal length.
Schmidt, W. C.↗
Conceptual nonorthogonal gyro configuration for guidance and navigation
Nonorthogonal sensor configuration using six single-degree-of-freedom inertial reference gyroscopes and a complete data processing and self-contained failure detection-and-isolation mechanism provides redundant capabilities to guidance and navigation systems. This system has been formulated in a strap-down configuration to attain maximum redundancy.
Gilmore, J. P.↗
Approach guidance system - Prototype computer program definition
Subroutines for prototype computer program definition for mathematical model of approach guidance system for estimating spacecraft orbit
Bennett, D. D.↗