Add to ORKGThe Space Launch System (SLS) Block-1B vehicle includes a low thrust-to-weight upper stage, which pr...
A market survey and evaluation of inertial guidance systems (inertial measurement units and digital ...
Guidance theory and trajectory analysis conference - research goals and programs in celestial mechan...
The main body of this paper describes the evolution of the Centaur D-1A Guidance and Software System...
Generalized equations and in-flight computer requirements for Centaur guidance and control and advan...
Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajector
Direct and indirect Atlas Centaur booster ascent mode comparisons for Mars flyby spacecraf
Summary of studies on guidance techniques and control equipment, spacecraft computers, and mathemati...
Guidance scheme for vehicle flight from lunar orbit to prescribed point on spherical nonrotating moo
A complete revision of the orbiter powered flight guidance scheme is presented. A unified approach t...
A guidance algorithm that provides precise rendezvous in the deterministic case while requiring only...
Apollo navigation and guidance - inertial measurement units and pulse torquing, optical measurements...
Design, development, and testing of inertial guidance and navigation systems for Apollo projec
Entry guidance equations, reference trajectories, and guidance system mechanizatio
A method is presented for open loop guidance of a solar electric propulsion spacecraft to geosynchro...
The Space Launch System (SLS) Block-1B vehicle includes a low thrust-to-weight upper stage, which pr...
A market survey and evaluation of inertial guidance systems (inertial measurement units and digital ...
Guidance theory and trajectory analysis conference - research goals and programs in celestial mechan...
The main body of this paper describes the evolution of the Centaur D-1A Guidance and Software System...
Generalized equations and in-flight computer requirements for Centaur guidance and control and advan...
Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajector
Direct and indirect Atlas Centaur booster ascent mode comparisons for Mars flyby spacecraf
Summary of studies on guidance techniques and control equipment, spacecraft computers, and mathemati...
Guidance scheme for vehicle flight from lunar orbit to prescribed point on spherical nonrotating moo
A complete revision of the orbiter powered flight guidance scheme is presented. A unified approach t...
A guidance algorithm that provides precise rendezvous in the deterministic case while requiring only...
Apollo navigation and guidance - inertial measurement units and pulse torquing, optical measurements...
Design, development, and testing of inertial guidance and navigation systems for Apollo projec
Entry guidance equations, reference trajectories, and guidance system mechanizatio
A method is presented for open loop guidance of a solar electric propulsion spacecraft to geosynchro...
The Space Launch System (SLS) Block-1B vehicle includes a low thrust-to-weight upper stage, which pr...
A market survey and evaluation of inertial guidance systems (inertial measurement units and digital ...
Guidance theory and trajectory analysis conference - research goals and programs in celestial mechan...