Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
A Simplified Guidance for Target Missiles Used in Ballistic Missile Defence Evaluation
Abstract A simplified guidance scheme for the target missiles used in Ballistic Missile Defence is presented in this paper. The proposed method has two major components, a Ground Guidance Computation (GGC) and an In-Flight Guidance Computation. The GGC which runs on the ground uses a missile model to generate attitude history in pitch plane and computes launch azimuth of the missile to compensate for the effect of earth rotation. The vehicle follows the pre launch computed attitude (theta) history in pitch plane and also applies the course correction in azimuth plane based on its deviation from the pre launch computed azimuth plane. This scheme requires less computations and counters In-flight disturbances such as wind, gust etc. quite efficiently. The simulation results show that the proposed method provides the satisfactory performance and robustness.
A Simplified Guidance for Target Missiles Used in Ballistic Missile Defence Evaluation
Abstract A simplified guidance scheme for the target missiles used in Ballistic Missile Defence is presented in this paper. The proposed method has two major components, a Ground Guidance Computation (GGC) and an In-Flight Guidance Computation. The GGC which runs on the ground uses a missile model to generate attitude history in pitch plane and computes launch azimuth of the missile to compensate for the effect of earth rotation. The vehicle follows the pre launch computed attitude (theta) history in pitch plane and also applies the course correction in azimuth plane based on its deviation from the pre launch computed azimuth plane. This scheme requires less computations and counters In-flight disturbances such as wind, gust etc. quite efficiently. The simulation results show that the proposed method provides the satisfactory performance and robustness.
A Simplified Guidance for Target Missiles Used in Ballistic Missile Defence Evaluation
Prabhakar, N. (Autor:in) / Kumar, I. D. (Autor:in) / Tata, S. K. (Autor:in) / Vaithiyanathan, V. (Autor:in)
01.01.2013
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
A Simplified Guidance for Target Missiles Used in Ballistic Missile Defence Evaluation
| Online Contents | 2013
Radar homing guidance for tactical missiles
| Tema Archiv | 1986
The Soviet Ballistic Missile and Space Flight Program
| NTIS | 1958
Optimal guidance for homing missiles: nose control and hit to kill
| British Library Conference Proceedings | 2000
| British Library Online Contents | 2011