Research on Multibody Dynamic Modeling and Simulation Technology for Launch Vehicles
Integrated Optimization Design of Base Structure/Piezoelectric Actuator Parameters for a Grid Reflector with Actuators
Influence Analysis of Nozzle Size on Flowfield and Thermal Environment in Arc heated Wind Tunnel
Maneuvering Estimation for Plane symmetric Aircraft Based on Destructive Time dependent Model
Observation Mission Planning for Maneuverable Satellite Constellation Towards Multiple Area Targets
Integrated Optimization of Navigation Features for Planetary Landing
Online Trajectory Planning for Launch Vehicles with Successive Convex Programming
Skip Entry Trajectory Optimization of Lunar Return Vehicles
Design of High Accuracy Scanning Mirror Control System with Large Inertia and Low Stiffness Connection
An Inter Satellite Link Autonomous Navigation Algorithm Based on Celestial Navigation Information Guidance
Identification and Analysis of Key Factors of Propellant Cross feed System in Launch Vehicle