Title :
An Analytic Solution of Entry Trajectory Based on Dynamic Pressure Planning
Author :
Wu, Liaoni ; Huang, Yimin ; He, Chenglong
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
Abstract :
An analytic trajectory solution based on dynamic pressure planning is presented for the gliding entry of lift-body. Firstly, the equations of motion are transformed from velocity to dynamic pressure and from time to altitude. An analytic method is proposed to calculate the trim angle-of-attack and other trajectory parameters based on dynamic pressure profile. Secondly, according the flight characteristics the entry is divided by initial descent and equilibrium glide. The dynamic pressure of equilibrium glide is scheduled and the geometric trajectory is calculated. Lastly, the simulation result shows that the trajectory design method is well satisfied the requirement of gliding entry.
Keywords :
position control; space vehicles; vehicle dynamics; analytic method; dynamic pressure planning; entry trajectory; equilibrium glide; geometric trajectory; trajectory design method; Aerodynamics; Design methodology; Differential equations; Dynamic scheduling; Earth; Technology planning; Trajectory; Transforms; Vehicle dynamics; Vehicles; Reentry; dynamic pressure planning; lift-body vehicle; trajectory design;
Conference_Titel :
Electronic Computer Technology, 2009 International Conference on
Conference_Location :
Macau
Print_ISBN :
978-0-7695-3559-3
DOI :
10.1109/ICECT.2009.36