Add to ORKGError analysis of celestial-inertial navigation for low thrust electrically propelled interplanetary space vehicle
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectorie
The article is devoted to mathematical models of errors of inertial navigation systems (INS). The ma...
A low-thrust guidance algorithm suitable for operational use was formulated. A constrained linear fe...
Trajectory calculations for Venus swingby trajectories, interplanetary navigation and guidance analy...
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Effect of bias errors on interplanetary navigation and guidance system performanc
Programmers manual for error propagation analysis in lunar and planetary trajectory tracking system
Methods which have been proposed to improve the navigation accuracy for the low-thrust space vehicle...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
Computer program for open-loop error analysis of low thrust interplanetary trajectorie
A lunar descent scheme with n periods of engine ON-OFF is investigated. Each period may have a diffe...
Analysis of error propagation in aircraft inertial guidance systems using flight simulation and math...
Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is...
Venus flyby, Mars flyby, and Mars orbital mission to evaluate navigation and guidance systems for ma...
An analysis was made of the guidance of a space vehicle approaching the earth at supercircular veloc...
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectorie
The article is devoted to mathematical models of errors of inertial navigation systems (INS). The ma...
A low-thrust guidance algorithm suitable for operational use was formulated. A constrained linear fe...
Trajectory calculations for Venus swingby trajectories, interplanetary navigation and guidance analy...
Digital computer program for performance analysis of all inertial guidance system along reference tr...
Effect of bias errors on interplanetary navigation and guidance system performanc
Programmers manual for error propagation analysis in lunar and planetary trajectory tracking system
Methods which have been proposed to improve the navigation accuracy for the low-thrust space vehicle...
An interplanetary low-thrust, solar electric propulsion mission simulation program suitable for navi...
Computer program for open-loop error analysis of low thrust interplanetary trajectorie
A lunar descent scheme with n periods of engine ON-OFF is investigated. Each period may have a diffe...
Analysis of error propagation in aircraft inertial guidance systems using flight simulation and math...
Strapdown inertial navigation system/celestial navigation system (SINS/CNS) integrated navigation is...
Venus flyby, Mars flyby, and Mars orbital mission to evaluate navigation and guidance systems for ma...
An analysis was made of the guidance of a space vehicle approaching the earth at supercircular veloc...
Lunar module navigation systems accuracies for powered descent, ascent, and abort trajectorie
The article is devoted to mathematical models of errors of inertial navigation systems (INS). The ma...
A low-thrust guidance algorithm suitable for operational use was formulated. A constrained linear fe...