CONTENTS

Policy on Intellectual Property Right (IPR)
1 Introduction
2 List of Annexes
Annex 1 Example of line-of-sight control and non-payload communication links characteristics for unmanned aircraft systems in the frequency bands 960-1 164 MHz and 5 000-5 150 MHz
1 First set of parameters (960-977 MHz and 5 030-5 091 MHz frequency bands)
2 Second set of parameters (5 000-5 150 MHz frequency band)
Annex 2 Example of beyond line-of-sight control and non-payload communication link characteristics for unmanned aircraft systems in the frequency bands 1 545-1 555 MHz (space-to-Earth), 1 610-1 626.5 MHz (space-to-Earth and Earth-to-space) and 1 646.5-1 656.5 MHz (Earth-to-space)
1 Frequency bands 1 545-1 555 MHz (space-to-Earth) and 1 646.5-1 656.5 (Earth-to-space)
2 Frequency band 1 610-1 626.5 MHz (space-to-Earth and Earth-to-space)
3 Examples of 1.5/1.6 GHz unmanned aircraft system link budgets
3.1 System 1
Satellite parameters
3.2 System 2
Annex 3 Example of beyond line-of-sight control and non-payload communication link characteristics for unmanned aircraft systems in the frequency band 5 030-5 091 MHz
1 Introduction
2 General architecture
3 Space segment
4 Unmanned aircraft terminal segment
5 Carrier bandwidth and frequency plan
6 Link budgets
Annex 4 Example of beyond line-of-sight control and non-payload communication link characteristics for unmanned aircraft systems in the frequency bands 12/14 GHz and 20/30 GHz
1 Unmanned aircraft system and geostationary orbit analysis methodology
1.1 Rain fade investigation
1.2 Provision for adjacent satellites
2 Unmanned aircraft system control and communications system characteristics
2.1 Information data rate
2.2 End-to-end link availability
2.3 Unmanned aircraft terminal parameters
2.4 Unmanned aircraft control station parameters
3 Using geostationary orbit satellites in the 12/14 GHz frequency bands for unmanned aircraft system control
3.1 12/14 geostationary orbit satellite characteristics
3.2 Uplink off-axis e.i.r.p. density and downlink power flux density
3.2.1 Uplink off-axis e.i.r.p. density limits
3.2.2 Downlink power flux density limits
3.3 12/14 GHz link budget calculation assumptions
3.3.1 Telecommand link budgets (unmanned aircraft control station-to-satellite and satellite-to-unmanned aircraft) (Links 1 and 2 of Fig. 4-2 below)
3.3.2 Telemetry link budgets (Unmanned aircraft-to-satellite and satellite-to-unmanned aircraft control station) (Links 3 and 4 of Fig. 4-2)
3.4 12/14 GHz link availability
3.4.1 Telecommand link (satellite-to-unmanned aircraft) rain fade margin
3.4.2 Telemetry link availability (unmanned aircraft-to-satellite) rain fade margin
3.5 Unmanned aircraft link budget summary for the frequency bands 12/14 GHz
4 Using geostationary orbit satellites in the 20/30 GHz frequency bands for unmanned aircraft system control
4.1 20/30 GHz geostationary orbit satellite characteristics
4.2 Uplink off-axis e.i.r.p. density and downlink power flux density
4.2.1 Uplink off-axis e.i.r.p. density
4.2.2 Downlink power flux density levels
4.3 20/30 GHz Link budgets calculation Assumptions
4.3.1 Telecommand link budgets (unmanned aircraft control station-to-satellite and satellite-to-unmanned aircraft) (links 1 and 2 of Fig. 4-2)
4.3.2 Telemetry link budgets (unmanned aircraft-to-satellite and satellite-to-unmanned aircraft control station) (Links 3 and 4 of Fig. 4-2)
4.4 20/30 GHz link availability
4.4.1 Telecommand link (satellite-to-unmanned aircraft) rain fade margin
4.4.2 Telemetry link availability (unmanned aircraft-to-satellite) rain fade margin
4.5 20/30 GHz frequency bands unmanned aircraft link budget summary
5 Potential interference to/from other satellite systems operating in the same frequency bands
Annex 5 Glossary