Low-Thrust Fuel-Optimal Rendezvous Mission to Near Earth Asteroids

Hao Huang; Zhong Xing Tang; Chao Han

doi:10.4028/www.scientific.net/AMR.816-817.778

Paper Titles

Design of Temperature Acquisition and Analysis System Based on LABVIEW
p.762

Short-Term Power Load Forecasting Based on Improved Wavelet Neural Network
p.766

Design on Elevate Mechanism of Large-Scale Multi-Stage Direct-Acting Hydraulic Hoist
p.770

A Novel Hybrid Unified Power Quality Conditioner (UPQC) for Medium-Voltage Power Grid
p.774

Low-Thrust Fuel-Optimal Rendezvous Mission to Near Earth Asteroids
p.778

Finite Element Analysis and Optimal Design of Commercial Vehicle Drive Axle Housing
p.782

Motion Analyses of D-Type Driving Mechanism
p.786

Structure Optimization of the Small Arm of Feed Mechanism in the Rubber Mixing Production Line
p.790

Thermo-Mechanical Reliability Evaluation of PLCC Packaging
p.795

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 816-817Low-Thrust Fuel-Optimal Rendezvous Mission to Near...

Low-Thrust Fuel-Optimal Rendezvous Mission to Near Earth Asteroids

Abstract:

Indirect method combined with homotopy approach is used to solve low-thrust fuel-optimal problem. To start the homotopy progress, pseudospectral method is used to solve energy-optimal problem to generate the initial guess. The proposed approach is applied to Earth to a near earth asteroid rendezvous mission. The performance of such approach is demonstrated through simulation.