The Lander Trajectory Reconstruction (LTR) computer program is a tool for analysis of the planetary entry trajectory and atmosphere reconstruction process for a lander or probe. The program can be divided into two parts: (1) the data generator and (2) the reconstructor. The data generator provides the real environment in which the lander or probe is presumed to find itself. The reconstructor reconstructs the entry trajectory and atmosphere using sensor data generated by the data generator and a Kalman-Schmidt consider filter. A wide variety of vehicle and environmental parameters may be either solved-for or considered in the filter process
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
textA navigation system for precision lunar descent and landing is presented and analyzed. The navig...
The recent development of manned and unmanned space vehicles has brought about an almost unprecedent...
The primary importance of trajectory reconstruction is to assess the accuracy of pre-flight predicti...
The Mars Entry Atmospheric Data System is a part of the Mars Science Laboratory, Entry, Descent, and...
The reconstruction of entry, descent and landing (EDL) trajectories is significantly affected by the...
This document describes the trajectory and atmosphere reconstruction of the Mars Phoenix Entry, Desc...
LANDER is a computer program used to predict the trajectory and flight performance of a spacecraft a...
The analysis has concerned itself with evaluating alternative methods of recovering a sample module ...
The objectives of this research were to develop a reconstruction capability using the Program to Opt...
A generalized covariance analysis technique which permits the study of the sensitivity of linear est...
Accelerometers are regularly flown on atmosphere-entering spacecraft. Using their measurements, the ...
A brief overview of statistical tools needed to perform post flight/test reconstruction of state var...
In the scope of this work, an extended Kalman filter is designed to enable INS/GPS (Inertial Navigat...
Accelerometers are regularly own on atmosphere-entering spacecraft. Using their measurements, the sp...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
textA navigation system for precision lunar descent and landing is presented and analyzed. The navig...
The recent development of manned and unmanned space vehicles has brought about an almost unprecedent...
The primary importance of trajectory reconstruction is to assess the accuracy of pre-flight predicti...
The Mars Entry Atmospheric Data System is a part of the Mars Science Laboratory, Entry, Descent, and...
The reconstruction of entry, descent and landing (EDL) trajectories is significantly affected by the...
This document describes the trajectory and atmosphere reconstruction of the Mars Phoenix Entry, Desc...
LANDER is a computer program used to predict the trajectory and flight performance of a spacecraft a...
The analysis has concerned itself with evaluating alternative methods of recovering a sample module ...
The objectives of this research were to develop a reconstruction capability using the Program to Opt...
A generalized covariance analysis technique which permits the study of the sensitivity of linear est...
Accelerometers are regularly flown on atmosphere-entering spacecraft. Using their measurements, the ...
A brief overview of statistical tools needed to perform post flight/test reconstruction of state var...
In the scope of this work, an extended Kalman filter is designed to enable INS/GPS (Inertial Navigat...
Accelerometers are regularly own on atmosphere-entering spacecraft. Using their measurements, the sp...
A nonlinear, six degree of freedom, digital computer simulation of a vehicle which has constant mass...
textA navigation system for precision lunar descent and landing is presented and analyzed. The navig...
The recent development of manned and unmanned space vehicles has brought about an almost unprecedent...