Add to ORKGThree-dimensional guidance scheme for decending from lunar orbit to hovering position based on linear theory of perturbation
The use of non-linear transformations is investigated in the context of an aero-assisted orbital tr...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...
Guidance scheme for vehicle flight from lunar orbit to prescribed point on spherical nonrotating moo
In recent years, NASA has indicated a desire to return humans to the moon. With NASA planning manned...
In recent years, NASA has indicated a desire to return humans to the moon. With NASA planning manned...
Spacecraft guidance technique for establishing lunar parking orbits using thrust vector control in r...
Visual simulation of lunar orbit establishment using simplified guidance techniqu
A 3-dimensional advanced guidance scheme is necessary to perform a successful precise lunar landing ...
Technique for thrust-vector orientation during manual control of lunar landings from synchronous orb...
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectorie
Trajectory requirements for terminal lunar landing from analog simulation of spacecraf
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The use of non-linear transformations is investigated in the context of an aero-assisted orbital tr...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...
Guidance scheme for vehicle flight from lunar orbit to prescribed point on spherical nonrotating moo
In recent years, NASA has indicated a desire to return humans to the moon. With NASA planning manned...
In recent years, NASA has indicated a desire to return humans to the moon. With NASA planning manned...
Spacecraft guidance technique for establishing lunar parking orbits using thrust vector control in r...
Visual simulation of lunar orbit establishment using simplified guidance techniqu
A 3-dimensional advanced guidance scheme is necessary to perform a successful precise lunar landing ...
Technique for thrust-vector orientation during manual control of lunar landings from synchronous orb...
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectorie
Trajectory requirements for terminal lunar landing from analog simulation of spacecraf
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The desire to return humans to the moon has motivated the evaluation of existing lunar descent guida...
The use of non-linear transformations is investigated in the context of an aero-assisted orbital tr...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control sy...