Finding Best Solution in Low-Thrust Trajectory Optimization by Two-Phase Homotopy

2018/09/14 by Binfeng Pan, Xun Pan, Ping Lu · 2 citations
Engineering · #Spacecraft Dynamics and Control #Space Satellite Systems and Control #Aerospace Engineering and Control Systems

paper · doi:10.2514/1.a34144

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

Cited by

• Three-Degree-of-Freedom Hypersonic Reentry Trajectory Optimization Using an Advanced Indirect Method
• Direct–Indirect Hybrid Strategy for Optimal Powered Descent and Landing

Related

• Multidisciplinary Design Optimization of Reusable Launch Vehicles for Different Propellants and Objectives
• Velocity Pointing Error Reduction for Spinning, Thrusting Spacecraft via Heuristic Thrust Profiles
• Preliminary Design of Multiple Gravity-Assist Trajectories
• Stage separation dynamics of spin-stabilized rockets
• Space Logistics Modeling and Optimization: Review of the State of the Art