Title :
Research of equilibrium-glide guidance method based on the generalized reference-trajectory
Author :
Liu, Jun ; Chen, Ke-jun ; Tang, Guo-Jian
Author_Institution :
Coll. of Aerosp. & Mater. Eng., Nat. Univ. of Defense Technol., Changsha, China
Abstract :
A new equilibrium-glide guidance method based on the generalized reference-trajectory was proposed for the glide phase of high lift-to-drag radio entry vehicles considering all path constrains. The 3DOF dynamic equations of high lift-to-drag radio entry vehicles were established, and the path constraints were specified. Then, the principle of the guidance method was explained in detail. At the same time, the basic guidance law was designed, and its longitudinal parameter was set by using the LQR (linear quadratic regular) method. Finally, the feasibility of this method was analyzed by emulation mode. Comparing from the former re-entry guidance method, the new guidance method adjusts the trajectory by the change of angle of attack, and the bank angle profile was small in the glide phase. The obtained results show that, the new guidance method can satisfy the glide guidance requirement of high lift-to-drag radio entry vehicles.
Keywords :
aerospace instrumentation; drag; space vehicles; 3DOF dynamic equations; bank angle profile; basic guidance law; emulation mode; equilibrium-glide guidance method; generalized reference-trajectory; glide phase; high lift-to-drag radio entry vehicles; linear quadratic regular method; longitudinal parameter; path constraints; re-entry guidance method; Aerodynamics; Earth; Equations; Mathematical model; Trajectory; Vehicle dynamics; Vehicles; LQR method; equilibrium-glide; generalized reference-trajectory; high lift-to-drag radio entry vehicles; re-entry guidance;
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4244-9617-4
DOI :
10.1109/RAST.2011.5966841