HALO  HALO Network


Broadband Wireless Services from High Altitude Long Operation
(HALO™) Aircraft

James N. Martina and Nicholas J. Colellab
aRaytheon TI Systems, MS 8497, 6600 Chase Oaks Blvd, Plano, TX 75023
bAngel Technologies, Magna Place, Suite 760, 1401 S Brentwood Blvd, St. Louis, MO 63144

Return to Main Page View other Technical Papers

 

 

Wireless Multimedia Interactivity via Stratospheric
HALO™ Aircraft

 

ABSTRACT

 

Broadband wireless millimeter wavelength services provided from a High Altitude Long Operation (HALO™) Aircraft are now feasible. Our talk will emphasize the conceptual design of a "bandwidth-on-demand" wireless network whose data rates to and from the subscriber will measure in the multi-megabit per second range. A variety of metropolitan area spectrum bands offer the needed bandwidth. An attractive choice is the LMDS band near 28 GHz and system characteristics at this frequency will be described.

 

The HALO™ Aircraft fuselage will house packet switching circuitry and fast digital network functions. The communications antenna and related components will be located in a pod suspended below the aircraft fuselage. To offer "ubiquitous" service throughout a large region, the HALO™ antenna will utilize multiple beams arranged in a typical cellular pattern. Broadband channels to subscribers in adjacent cells will be separated in frequency. As the beams traverse over a user location, the virtual path through the packet switch will be changed to perform a beam-to-beam handoff.

 

Introduction

The convergence of innovative technologies and manufacturing capabilities affecting aviation, millimeter wave wireless, and multi-media communications industries enables Angel Technologies Corporation and its partners to pursue new wireless broadband communications services. The HALO™ Network will offer ubiquitous access to any subscriber within a "super metropolitan area" from an aircraft operating at high altitude. The aircraft will serve as the hub of the HALO™ Network serving tens to hundreds of thousands of subscribers. Each subscriber will be able to communicate at multi-megabit per second data rates through a simple-to-install subscriber unit. The HALO™ Network will be steadily evolved at a pace with the emergence of data communications technology world-wide. The HALO™ Network will be a universal wireless communications network solution. It will be deployed globally on a city-by-city basis.

 

The nature of the equipment needed for this broadband wireless service is evolutionary, not revolutionary. Most of the technology already exists. The engineering effort will focus primarily on adapting and integrating components and subsystems from terrestrial markets to offer a complete network solution. Proven technology will be used to the maximum extent. Since the HALO™ Aircraft operate from regional airports, the equipment will be routinely maintained and calibrated. The operating plan assumes equipment upgrades as technology advances yield lower cost and weight and provide increased performance.

 

A Broadband Wireless Metropolitan Area Network

An airplane specially designed for high altitude flight with a payload capacity of approximately one ton is being developed for commercial wireless services. It will circle at high altitudes for extended periods of time and it will serve as a stable platform from which broadband communications services will be offered. The High Altitude Long Operation (HALO™) Aircraft will maintain station at an altitude of 52 to 60 thousand feet by flying in a circle with a diameter of about 5 to 8 nautical miles. Three successive shifts on station of 8 hours each, for example, can provide continuous service for 24 hours per day, 7 days per week. Such a system can cost-effectively provide broadband multimedia communications to diverse business groups and to the general public.

If a viewing angle of 20 degrees or higher is chosen to facilitate good line-of-sight coverage at millimeter wave (MMW) frequencies (20 GHz or higher), one such platform will cover an area of approximately 2800 square miles encompassing a typical metropolitan area. Operation at MMW frequencies enables broadband systems to be realized, by providing spectrum bandwidths of 1 to 6 GHz. MMW systems also permit very narrow beamwidths to be realized with small aperture antennas.

 



The HALO™ Network can utilize a cellular pattern on the ground so that each cell uses one of four frequency sub-bands, each having a bandwidth up to 60 MHz each way. A fifth sub-band can be used for gateways (connections to the public network or to dedicated users). Each cell will cover an area of a few square miles. The entire bandwidth will be reused many times to achieve total coverage throughout the 2800 square mile area served by the airborne platform. The total capacity of the network supported by a single airborne platform can be greater than 100 Gbps. This is comparable to terrestrial fiber-optic (FO) networks and can provide two-way broadband multimedia services normally available only via FO networks.

 

The HALO™ Network provides an alternative to satellite- and ground-based communications systems. Unlike satellite systems, however, the airborne system concentrates all of the spectrum usage in certain geographic areas, which minimizes frequency coordination problems and permits sharing of frequency with ground-based systems. Enough power is available from the aircraft power generator to allow broadband data access from small user terminals.

A New Layer in the Wireless Infrastructure

Raytheon Systems Company and Angel Technologies Corporation have the opportunity to serve the growing wireless communications market by using a HALO™ Aircraft that transmits high-speed data traffic throughout a metropolitan region. The goal is to interconnect more than 100,000 subscribers within a metropolitan center and its surrounding communities through a star topology network. This HALO™ Network has the benefits of low cost, high flexibility, and high quality of service.

 

HALO™ Aircraft provide a new layer in the traditional hierarchy of wireless communications. The HALO™ Network can be thought of as a "tall tower" approach that provides better line of sight to customers without the high cost of deploying and operating a satellite constellation.

 

Terrestrial Towers

< 200 feet

HALO™ Aircraft

10 miles

Low Earth Orbit (LEO) Satellites

400 miles

Geostationary Earth Orbit (GEO) Satellites

22,300 miles

 

This paper will describe the architecture and the concept of operations of the HALO™ Network. It will also describe key characteristics of the HALO™ Aircraft, the communications payload, and subscriber units. An earlier paper2 entitled "The Cone of Commerce™" covered the business and market aspects of the HALO™ Network. The paper by Djuknic3 provides an overview of the various options and highlights the unique advantages of stratospheric platforms for providing wireless communications services.

 

The HALO™ Network Concept

Overview

The attributes of the HALO™ Network are illustrated in the figure on the next page. Many types of subscribers—schools, families, hospitals, doctors’ offices, and small to medium size businesses—will benefit from the low price of HALO™ Network broadband services.

 

The equipment will connect to existing networks and telecommunications equipment using standard broadband protocols such as ATM and SONET. The HALO™ Gateway provides access to the Public Switched Telephone Network (PSTN) and to the Internet backbone for such services as the World Wide Web and electronic commerce.

Key Features

The key features of the HALO™ Network are summarized below:

  • Seamless ubiquitous multimedia services

  • Adaptation to end user environments

  • Enhanced user connectivity globally

  • Rapidly deployable to sites of opportunity

  • Secure and reliable information and data transactions

  • Bandwidth on demand for efficient use of available spectrum


There are various classes of service to be provided: (a) 1-5 Mbps communication links to consumers; and (b) 5-12.5 Mbps links for business users. Since the links would be bandwidth-on-demand, the total available spectrum would be shared between concurrent active sessions. The nominal data rates would be low while the peak rates would expand to a specified level. A gateway type service can be provided for dedicated links at 25-155 Mbps.

 

Based on the LMDS spectrum and 5-fold reuse, the service capacity would be 10,000 to 75,000 simultaneous, symmetrical T1 circuits (1.5 Mbps) per Communications Payload. The HALO&#153; Aircraft would provide urban and rural coverage from a single platform to provide service to:

  • 100-750,000 subscribers
  • 40-60 mile diameter service area
  • (1,250 to 2,800 square miles)


Network Access Various methods for providing access to the users on the ground are feasible. The figure below shows one approach where each spot beam from the payload antenna serves a single cell on the ground in a frequency-division multiplex fashion with 5-to-1 frequency reuse, four for subscriber units and the fifth for gateways to the public network and to high-rate subscribers. Other reuse factors such as7:1 and 9:1 are possible. Various network access approaches are beinexplored.


Image3.gif (15195 bytes)

Network Services

The HALO™ node provides a multitude of connectivity options as shown on the next page. It can be used to connect physically separated Local Area Networks (LANs) within a corporate intranet through frame relay adaptation or directly through LAN bridgers and routers. Or it can provide videoconference links through standard ISDN or T1 interface hardware. The HALO™ Network may use standard SONET and ATM protocols and equipment to minimize the cost of the equipment and to take advantage of the wide availability of these components.

 

 

 

HALO™ Network Architecture

 

At the apex of a wireless Cone of Commerce™, the payload of the HALO™ Aircraft becomes the hub of a star topology network for routing data packets between any two subscribers possessing premise equipment within the service coverage area. A single hop with only two links is required, each link connecting the payload to a subscriber. The links are wireless, broadband and line of sight. Single link delays range from ~50 msec under the airplane to ~200 msec at the edge of the signal footprint.

 

Information created outside the service area is delivered to the subscriber’s consumer premise equipment (CPE) through business premise equipment (BPE) operated by businesses, Internet Service Providers (ISPs), or content providers within that region, and through the HALO™ Gateway ("HG") equipment directly connected to distant metropolitan areas via leased trunks. The HG is a portal serving the entire network. It avails system-wide access to content providers or advertisers, and it allows any subscriber to extend their communications beyond the HALO™ Network service area by connecting them to dedicated long-distance lines such as inter-metro optical fiber.

 

 


As with all wireless millimeter wave links, high rainfall rates can reduce the effective data throughput of the link to a given subscriber. Angel plans to ensure maximum data rates more than 99.7% of the time, reduced data rates above an acceptable minimum more than 99.9% of the time, and to limit outages to small areas (due to the interception of the signal path by very dense rain columns) less than 0.1% of the time. Angel plans to locate the HG close to the HALO™ orbit center to reduce the slant range from its high-gain antenna to the aircraft and hence its signal path length through heavy rainfall.

HALO™ Aircraft

 

The HALO™ Aircraft is under development and flight testing will occur by September-1998. The aircraft has been specially designed for the HALO™ Network with the Communications Payload Pod suspended from the underbelly of its fuselage.

 

 

 

 

 

 

 

 

The HALO™ Aircraft will fly above the metropolitan center in a circular orbit of five to eight nautical miles diameter. The Communications Payload Pod is mounted to a pylon under the fuselage. As the aircraft varies its roll angle to fly in the circular orbit, the Communications Payload Pod will pivot on the pylon to remain level with the ground. Other details on the aircraft can be found in the Cone of Commerce™ paper.2

Communications Payload

 

The HALO™ Network will use an array of narrow beam antennas on the HALO™ Aircraft to form multiple cells on the ground. Each cell covers a small geographic area, e.g., 4 to 8 square miles. The wide bandwidths and narrow beamwidths within each beam or cell are achieved by using MMW frequencies. Small aperture antennas can be used to achieve small cells. A more detailed description of the communications payload equipment is given in another technical paper.1

 

Subscriber Units

 

A block diagram describing the CPE (and BPE) is shown below. It entails three major sub-groups of hardware: the RF Unit (RU) which contains the MMW Antenna and MMW Transceiver; the Network Interface Unit (NIU); and the application terminals such as PCs, telephones, video servers, video terminals, etc. The RU consist of a small dual-feed antenna and MMW transmitter and receiver which is mounted to the antenna. An antenna tracking unit uses a pilot tone transmitted from the HALO™ Aircraft to point its antenna at the airplane.

 

The MMW transmitter accepts an L-band (950 - 1950 MHz) IF input signal from the NIU, translates it to MMW frequencies, amplifies the signal using a power amplifier to a transmit power level of 100 - 500 mW of power and feeds the antenna. The MMW receiver couples the received signal from the antenna to a Low Noise Amplifier (LNA), down converts the signal to an L-band IF and provides subsequent amplification and processing before outputting the signal to the NIU. Although the MMW transceiver is broadband, it typically will only process a single 40 MHz channel at any one time. The particular channel and frequency is determined by the NIU.

 

The NIU interfaces to the RU via a coax pair which transmits the L-band TX and RX signals between the NIU and the RU. The NIU comprises an L-band tuner and down converter, a high-speed (up to 60 Mbps) demodulator, a high-speed modulator, multiplexers and demultiplexers, and data, telephony and video interface electronics. Each user terminal will provide access to data at rates up to 51.84 Mbps each way. In some applications, some of this bandwidth may be used to incorporate spread spectrum coding to improve performance against interference (in this case, the user information rate would be reduced).

 

The NIU equipment can be identical to that already developed for LMDS and other broadband services. This reduces the cost of the HALO™ Network services to the consumer since there would be minimal cost to adapt the LMDS equipment to this application and we could take advantage of the high volume expected in the other services. Also, the HALO™ RU can be very close in functionality to the RU in the other services (like LMDS) since the primary difference is the need for a tracking function for the antenna. The electronics for the RF data signal would be identical if the same frequency band is utilized.

 

The subscriber equipment can be readily developed by adapting from existing equipment for broadband services.

Summary

 

The HALO™ Network is capable of providing high rate communications to users of multimedia and broadband services. The feasibility of this approach is reasonably assured due to the convergence of technological advancements. The key enabling technologies at hand include:

 

GaAs (Gallium Arsenide) RF devices which operate at MMW frequencies

ATM/SONET Technology and Components

Digital Signal Processing for Wideband Signals

Video Compression

Very Dense Memory Capacity

Aircraft Technology

These technologies are individually available, to a great extent, from commercial markets. The HALO™ Network seeks to integrate these various technologies into a service of high utility to small and medium businesses and other multimedia consumers at a reasonable cost.

 

Acknowledgments

 

The authors wish to thank J. Leland Langston for providing his valuable inputs and many discussions on this topic.

 

REFERENCES

 

J. Martin and N. Colella, "Broadband Wireless Services from High Altitude Long Operation (HALO™) Aircraft," Proc. of the SPIE International Symposium on Voice, Video, and Data Communications: Broadband Engineering for Multimedia Markets, 1997.

N. Colella and J. Martin, "The Cone of Commerce™," Proc. of the SPIE International Symposium on Voice, Video, and Data Communications: Broadband Engineering for Multimedia Markets, 1997.

G. Djuknic, J. Freidenfelds, et al., "Establishing Wireless Communications Services via High-Altitude Aeronautical Platforms: A Concept Whose Time Has Come?," IEEE Communications Magazine, September 1997.

 

BIOGRAPHIES

 

James Martin is the lead systems engineer and project manager for the HALO™ communications payload under development at Raytheon Systems Company for Angel Technologies. At AT&T Bell Labs, he developed cellular wireless telecommunications equipment and underwater fiber optic transmission systems. Mr. Martin has recently published a "Systems Engineering Guidebook" with the CRC Press. His specialty is systems engineering management, systems architecting and the total systems engineering process.

 

Dr. Nicholas J. Colella is the Chief Technology Officer of Angel Technologies Corporation. In prior years, he held senior technical positions at Lawrence Livermore National Laboratory. He invented the RAPTOR/TALON theater ballistic missile defense concept and served as DOD’s executing agent for pioneering low-cost, high-altitude, long-endurance unmanned aircraft, high mass fraction kinetic kill interceptors, electro-optics and communications systems. He co-created Brilliant Pebbles, led LLNL’s spacecraft design and survivability projects, and developed one-steradian wide field of view (WFOV) cameras employing spherically concentric refractive optics for tracking satellites and space objects. He is a founding partner of a multi-chip module company and the National Robotics Engineering Consortium at Carnegie Mellon.

 

TABLE OF CONTENTS

1. BACKGROUND

1.1 Introduction

1.2 A Broadband Wireless Metropolitan Area Network

1.3 A New Layer in the Wireless Infrastructure

2. THE HALO™ NETWORK CONCEPT

2.1 Overall Concept

2.2 Key Features

2.3 Service Attributes

2.3.1 Network Access

2.3.2 Network Services

3. HALO™ NETWORK ARCHITECTURE

4. HALO™ AIRCRAFT

5. COMMUNICATIONS PAYLOAD

6. SUBSCRIBER UNITS

7. SUMMARY

 

TABLE OF FIGURES

HALO™ Aircraft Provides Wireless Broadband Services over Metropolitan Centers

High-Speed Data Links Transmitted Over Millimeter Wave Frequencies Provide Broadband Data Services to Various End-Users

Cell Coverage by Frequency Division Multiplexing using Spot Beams

The HALO™ Network Accommodates a Variety of Interfaces

The HALO™ Network

HALO™ Aircraft with Suspended Communications Payload

Functional Block Diagram of the Subscriber Equipment

 

Acknowledgments

The authors wish to thank J. Leland Langston for providing his valuable inputs and many discussions on this topic.

REFERENCES

  1. N. Colella and J. Martin, "The Cone of Commerce™," Proc. of the SPIE International Symposium on Voice, Video, and Data Communications: Broadband Engineering for Multimedia Markets, 1997.
  2. G. Djuknic, J. Freidenfelds, et al., "Establishing Wireless Communications Services via High-Altitude Aeronautical Platforms: A Concept Whose Time Has Come?," IEEE Communications Magazine, September 1997.

BIOGRAPHIES

 


Top of Page
| Return to Home PageView other Technical Papers

 

Copyright 1997-1998, Angel Technologies Corporation. All Rights Reserved.

Website hosting by voltage.com