Title :
Resident trajectory optimization for stratospheric Airships
Author :
Zhu Ming ; Li Leiyun ; Guo Xiao ; Zheng Zewei
Author_Institution :
Sch. of Aeronaut. Sci. & Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Abstract :
Resident trajectory optimization is addressed for a stratospheric Airship. The equations of motion for the airship include the factors about aerodynamic force, added mass and wind profiles are developed based on horizontal-wind model. For minimum penalty which consists of the resident error, the derivative of state variables and the energy cost during resident, a trajectory optimization problem is constructed and then converted into a dynamic programming problem by a reinforcement learning (RL) method. In different scenarios, the optimal trajectory is found by the receding horizon differential dynamic programming (RH-DDP). For the minimum resident penalty trajectory, the RH-DDP solutions which have a 57.85% and 67.3% CUP idle rate in the two cases, state that the RH-DDP method can satisfy the demands of real-time computation during resident.
Keywords :
aerospace computing; airships; dynamic programming; learning (artificial intelligence); trajectory optimisation (aerospace); vehicle dynamics; CUP idle rate; RH-DDP method; RL method; added mass; aerodynamic force; energy cost; equations of motion; horizontal-wind model; minimum resident penalty trajectory; optimal trajectory; receding horizon differential dynamic programming; reinforcement learning method; resident error; resident trajectory optimization problem; state variable derivative; stratospheric airships; wind profiles; Dynamic programming; Equations; Force; Mathematical model; Optimization; Trajectory; Vectors; Airship; receding horizon differential dynamic programming; residence; trajectory optimation;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896509