Launch vehicle error sensitivity study
Booster trajectory optimization for launch vehicle range sensitivity analysis
Rosenbaum, R. C.↗
Engineering topics
Publications and source records attributed to Willwerth, R. E..
Booster trajectory optimization for launch vehicle range sensitivity analysis
Steepest descent method of trajectory optimization for computing lunar and interplanetary transfer missions, noting terminal constraints
Steepest descent method to compute powered flight trajectory optimization for lunar and interplanetary transfer