Amanote Research
Register
Sign In
Fuel-Efficient Descent and Landing Guidance Logic for a Safe Lunar Touchdown
doi 10.2514/6.2011-6499
Full Text
Open PDF
Abstract
Available in
full text
Date
August 8, 2011
Authors
Allan Lee
Publisher
American Institute of Aeronautics and Astronautics
Related search
Guidance of Reusable Launchers: Improving Descent and Landing Performance
Journal of Guidance, Control, and Dynamics
Control
Systems Engineering
Electronic Engineering
Applied Mathematics
Space
Electrical
Planetary Science
Aerospace Engineering
Systematic Performance-Oriented Guidance Tuning for Descent & Landing on Small Planetary Bodies
Acta Astronautica
Aerospace Engineering
Enhancements on the Convex Programming Based Powered Descent Guidance Algorithm for Mars Landing
SPARTAN: A Novel Pseudospectral Algorithm for Entry, Descent, and Landing Analysis
KOREAN LUNAR LANDER &Ndash; CONCEPT STUDY FOR LANDING-SITE SELECTION FOR LUNAR RESOURCE EXPLORATION
ISPRS - International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences
Generalized Hp Pseudospectral-Convex Programming for Powered Descent and Landing
Journal of Guidance, Control, and Dynamics
Control
Systems Engineering
Electronic Engineering
Applied Mathematics
Space
Electrical
Planetary Science
Aerospace Engineering
Vision-Aided Inertial Navigation for Spacecraft Entry, Descent, and Landing
IEEE Transactions on Robotics
Control
Systems Engineering
Computer Science Applications
Electrical
Electronic Engineering
Probabilistic Hazard Detection for Autonomous Safe Landing
Hybrid Optimization of Powered Descent Trajectory for Manned Lunar Mission
Transactions of the Japan Society for Aeronautical and Space Sciences
Space
Planetary Science
Aerospace Engineering