Arizona State University

Ground Effects

Advanced Helicopter Electromagnetics Laboratory | Comments

Analysis of antennas on a helicopter airframe including the surrounding environment, such as the ground, will provide much more reliable radiation characteristics for communication link budget predictions. In order to account for all reflections and diffractions from the airframe, as well as those from a stratified ground, a full-wave analysis should be used. Since the exact Green's function for a stratified ground is available, the radiation problem of a helicopter above the ground reduces to a problem of finding the total equivalent source in the presence of the ground. Furthermore, if the observation points are confined only in the upper hemisphere, then the asymptotic solution for the radiated field due to the source can be obtained by using the Reflection Coefficient Method (RCM) or Norton's approximation.

In this study, the ground influence on the radiation pattern is investigated using the Finite Element Method (FEM) in conjunction with Norton's approximation. Therefore, the radiated field contains not only the space wave but also the surface wave which is important for a short observation distance. The lossy ground is defined by its relative permittivity and electric conductivity. To illustrate the capability of the method, the radiated fields due to the VHF/HF antenna on a helicopter model are predicted. As for the VHF antenna, a 12.75-cm monopole mounted on the NASA scaled helicopter model is investigated when its height from different grounds is varied. In addition, HF antennas, such as a 14-ft towel-bar and a 24-ft inverted-L on the AH-64 (Apache) full-scale helicopter, are analyzed in the presence of sea water or a stratified ground.




Figure 1: Apache full-scale helicopter model with a 14 ft towel-bar antenna on the left hand side and a 24-ft inverted-L antenna on the right hand side both of which are used at the HF band.



Figure 2: Influence of soil type ground on the pitch-plane radiation pattern when a 12.75-cm VHF monopole is mounted on the NASA scale model.



Figure 3: The space and the surface wave arising from a 14-ft towel-bar antenna on the Apache full-scale model when the helicopter is flying over sea.

[ Summary | Research Activities | Electromagnetic Computational Methods and Computer Codes | X-Window Interfaces | Composite Materials | Cosite Interference | Rotor Modulation | Lightning Effects on Aircraft | Antenna Technology | HIRF | Conferences/Meetings | AHE Research Team ]

All rights reserved. All trademarks mentioned herein belong to their respective owners.

Webmaster

AHE