Paper Title:
Design of the Scheme Flight Trajectory Command for the Tactical Missile
  Abstract

For the case of the scheme trajectory command design for the tactical missile, the longitudinal and lateral commands and the compound controller of the attitude and height were designed. In the launch segment, four kinds of heading angle commands were presented adopting the arc method and reduction law. In the variable height flight segment, two kinds of height commands were gained by using the parabolic and exponential function. Considering the earth curvature, the formula of the great circle course and distance was gotten applying spherical triangle solution method, and the flight command along the route dot in the lateral plane was obtained. The simulation results show that the designed scheme trajectory commands are feasible and effectively.

  Info
Periodical
Key Engineering Materials (Volumes 480-481)
Edited by
Yanwen Wu
Pages
1426-1431
DOI
10.4028/www.scientific.net/KEM.480-481.1426
Citation
Y. T. Zhao, Y. A. Hu, "Design of the Scheme Flight Trajectory Command for the Tactical Missile", Key Engineering Materials, Vols. 480-481, pp. 1426-1431, 2011
Online since
June 2011
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Tao Jiang, Di Xiao Wu, Li Rui
Abstract:Under the condition of compendium preparation of shooting data,based on the correlation of each torpedo catching target during torpedo salvo,...
488
Authors: Yan Ming Lu
Chapter 2: Simulation and Engineering Optimization
Abstract:As to spiral groove grinding, a formed wheel was needed to be designed and manufactured conventionally based on envelope theory, and then...
207
Authors: Song Mo, Jun Huang, Xue Chai, Quan Zhao
Chapter 7: Manufacturing Process Planning and Scheduling
Abstract:The take-off control of UAV with fly wing layout is limited by its relatively lower pitch moment. This paper gained the state parameters of a...
265
Authors: Jun Wei Li, Hui Jiang
Chapter 16: Auto-Detection Technology
Abstract:Vehicle reference model with two degree of freedom and multi-body vehicle dynamic model are set up at first. This paper presents a Fuzzy...
1939
Authors: Zhi Ping Li, Jun Zhou, Jian Guo Guo
Chapter 1: Research and Engineering in the Field of Control and Intelligent Systems
Abstract:A new nonlinear robust guidance law was proposed by considering autopilot dynamics. Firstly, the mathematic model was built according to...
77