Optimal Terminal Descent Guidance Logic to Achieve a Soft Lunar Touchdown
LUNAR AND PLANETARY SOFT LANDINGS BY MEANS OF GAS-FILLED BALLOONS
Minimum-fuel, two-impulse, soft lunar landing orbits
Highlights of the press conference at the Moscow House of Scientists on 10 February 1966
On touchdown dynamics analysis for lunar landing.
The Analysis and Configuration of a Control System for a Mars Propulsive Lander
Monte Carlo approach to touchdown dynamics for soft lunar landings
Soviet press communiques and the Pravda editorial on ''Luna-9'' soft landing on the moon
Design considerations for Surveyor guidance.
Propellant requirements for unmanned lunar and interplanetary soft landing vehicles.
Propellant requirements for unmanned lunar and interplanetary soft landing vehicles.
Energy dissipating structures - A structures materials design synthesis
The analysis and configuration of a control system for a Mars propulsive lander.
Closed loop ''optimal'' guidance equations for soft landing