dvac concept description: offset gregorian ......dvac concept description: offset gregorian dish —...
TRANSCRIPT
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DVAC CONCEPT DESCRIPTION:
OFFSET GREGORIAN DISH — DVAC-1PRIME FOCUS DISH — DVAC-2
杜彪 (Biao Du), Chief Eng.彭勃 (Bo Peng), Director @JLARTJoint Lab. for Radio Astronomy and TechnologyJuly 15, 2011, Penticton
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1. Dish Verification Antenna China in General2. DVAC Design Principle3. DVAC-1 Main Specifications 4. DVAC-1 Concept Design 5. DVAC-1 Main Specification Budget 6. DVAC-2 Specs7. DVAC-2 Concept Design8. DVAC-2 Specification Budget
Outline
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1. DVAC General
Potentially three types of reflector antenna could be used:
Prime focus reflector antenna
Dual symmetric reflector
Dual offset reflector
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A prime focus reflector antenna has advantage of the simplest optical design, a symmetry helps the mechanical design and low cost. But disadvantages are:
1. DVAC General
Prime focus reflector antenna
impossible to simultaneously optimize aperture efficiency and noise temperature;
lower efficiency and higher side-lobe due to larger blockage;
mechanically difficult to accommodate multiple feeds and a PAF at the primary focus.
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Aadvantages• Shaping produce high aperture efficiency and low noise T; • Feed spillover pointing to sky further reduce noise temperature;• Symmetry helps with mechanical design and cost.
Disadvantages• Subreflector has to be small to reduce aperture blockage, limiting
the low frequency performance; • Small subreflector requires high gain (narrow beam) feeds, limiting
use of broadband feeds with wide angle illumination; • Lower frequency feed and PAF to be at the primary focus, requiring
a feed interchange mechanism, difficult to accommodate two feedsat the primary focus.
1. DVAC General
Dual symmetric reflector antenna
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Advantages• Shaping produce high aperture efficiency and low noise T; • No blockage design further enhances aperture efficiency and reduces
wide angle sidelobes; • Feed spillover pointing at the sky can further reduce the noise
temperature; • Mechanically easy to accommodate multiple feeds at the secondary
focus and a PAF at the primary focus.
Disadvantages asymmetry increases the complexity of mechanical design leading to higher costs.
1. DVAC General
Dual offset reflector antenna
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1. DVAC General
Dish Verification Antenna China #1 (DVAC-1) refers to an offset Gregorian dish;
DVAC-2 refers to an axis-symmetric dish (prime focus reflector antenna).
JLRAT propose two concept designs for the SKA dish.
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1. DVAC General
SKA Dish Verification Antenna: Executive Summary
SKA Dish Verification Antenna System Functional Specifications
Requirements_spreadsheet_v1_20100929(1)
Reference
Main specifications and Concept Design
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Excellent performance
Low cost
Ease of transportation and installation
Minimal routine maintenance
Long lifetime
2. Design Principle
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DVAC CONCEPT DESCRIPTION:
OFFSET GREGORIAN DISH — DVAC-1
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Antenna Type Offset-Gregorian Antenna , Diameter 15m
Mount Type EL over AZ (AZ:Gear,EL: Screw)Frequency Band 0.3GHz ~ 10GHz
Frequency Band Switch Manner Switching Feeds within 30s
Surface Accuracy of Main Reflector≤1.2 mm RMS (at night, under low wind)≤1.25mm RMS (Wind 7m/s , ΔT=5ºC)≤1.75mm RMS (Wind 20m/s , ΔT=7ºC)
Pointing Accuracy≤10 arcsec RMS (at night and no wind)
TBC (at daytime, with wind)Antenna Aperture Efficiency (%) ≥ 55%First Sidelobe Level ≤-18dB
3. Main Specifications for DVAC-1
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Polarization Dual-LP/Dual-CP Travel Range AZ:±270°, EL:15°∼ 85°Slew Rates (Max) AZ:3°/s, El:1°/sAcceleration (Max) AZ:3°/s2, El:1°/s2
Wind Velocity Drive to stow :70 km/hSurvival: 160 km/h (at El=54°)
Design Lifetime ≥ 30 years
3. Main Specifications for DVAC-1
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4. Concept DesignMain Attractions of DVAC-1 Design
Offset-Gregorian Antenna
Wide Band Feed (WBF)
Integrated Modular Design
Integrated Main Reflector Surface (Single Panel)
Sealed and Lubricated Driving Devices
Mature Technology
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Design and Manufacture4. Concept Design
Block Diagram of 15 Meter Antenna System
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(1) Microwave Optical Design
(2) Structure Design
(3) Servo Control Design
4. Concept Design
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4. Concept Design(1) Microwave Optical Design
Feed Design
Main and Sub Reflector Curve Design
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Feed DesignOperating frequency: 0.3GHz~10GHz (33 octaves)
4. Concept Design(1) Microwave Optical Design
two wide-band feeds (WBF)
WBF advantages:
Bandwidth of several octaves;
Dual linear or circular polarization
Constant phase centre
Equal E- and H-plane beamwidth
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4. Concept Design(1) Microwave Optical Design
Feed DesignFeed 1(0.3GHz ~ 1.5GHz ) and Feed 2(1.5GHz ~ 10GHz )
Eleven Feed
Simulation Model
Frequency(GHz)
Length×Width×Height(mm)
Weight(kg)
0.3~1.5 1040×1040×350 20
1.5~10 250×250×120 8
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4. Concept Design(1) Microwave Optical Design
Feed Design
Radiation Patterns of Feed1 at 0.3, 0.9 and 1.5GHz
Radiation Patterns of Feed2 at 1.5, 6 and 10GHz
Illuminating range
Illuminating range
Subreflector Edge Taper: -9 ~ -15dB
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4089
55°55°
4357
1712
18733
15000
34.7°
Optimum Design
Main and Sub Reflector Curve Design
55°Opening Angle-13dB Feed Edge Taper
4. Concept Design(1) Microwave Optical Design
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-20 -15 -10 -5 0 5 10 15 20-50
-45
-40
-35
-30
-25
-20
-15
-10
-5
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
Freq=0.3GHz Taper=-13dB
phi=0°phi=90°
-10 -8 -6 -4 -2 0 2 4 6 8 10-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
Freq=1.5GHz Taper=-13dB
phi=0°phi=90°
-5 -4 -3 -2 -1 0 1 2 3 4 5-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
Freq=6GHz Taper=-13dB
phi=0°phi=90°
-3 -2 -1 0 1 2 3-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
Freq=10GHz Taper=-13dB
phi=0°phi=90°
4. Concept Design(1) Microwave Optical Design
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Radiation Performance of Antenna with PAF at Prime Focus
θ (angle)
θ (angle)
PAF at Position No. 7 PAF at Position No. 6
PAF at Original Focus
4. Concept Design(1) Microwave Optical Design
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lnitial Design
Current DesignSingle PanelSimple StructureLight WeightLow CostFast Installation
4. Concept Design(2) Structure Design
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Reflector Design
Mount Design
Structural Mechanics Analysis
4. Concept Design(2) Structure Design
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Single integrated main reflector
Minimal spar structure
Turning head design with a lead screw elevation actuator
Support and interchange mechanism for a PAF and 3 SPFs or 2 WBFs.
4. Concept Design(2) Structure Design
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Reflector Design
Main reflector
Back structure
Subreflector
Feed switch mechanism
4. Concept Design(2) Structure Design
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Reflector Design — Main reflectorDesign 1: Aluminum sandwich structureSingle aluminium panelSkins: 2mm (upper)/1mm (lower) in thickness, 2m in widthSkin and ribs are glued through negative pressure method on mould Surface accuracyσ≤0.8mm
Rib Configuration
4. Concept Design(2) Structure Design
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Reflector Design — Main reflector
Design 2: Carbon fibre sandwich structure
Single carbon fibre panelCarbon fibre skins: 1.5mm (top)/1mm (bottom) in thickness
Polyurethane foam: in the middle
Surface accuracyσ≤0.8mm
4. Concept Design(2) Structure Design
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Reflector Design — Back structure
The backup structure is based on US TDP design with some modifications (some details see to DVAC-1).
4. Concept Design(2) Structure Design
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Reflector Design — Subreflector
Magnesium material, 30% lighter than aluminum alloy. Surface accuracy σ≤0.25mm
4. Concept Design(2) Structure Design
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Reflector Design — Feed Switch Mechanism
4. Concept Design(2) Structure Design
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Elevation Part
Azimuth Part
Pedestal
Mount Design
4. Concept Design(2) Structure Design
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Mount Design — Azimuth part
Dual-motor anti-backlash driveExternal gear bearing, easy to
maintainSeal cover is used to exclude
dust and sand
4. Concept Design(2) Structure Design
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Mount Design — Elevation partA planetary reducer with a ball screw drive is used
for the elevation part without a counterweight.
4. Concept Design(2) Structure Design
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Mount Design
A flexible-axis drive technique is adopted for Az and EI encoder mechanism.
A double-layer ring structure is used for AZ cable wrap.A modular design for all rotating parts.A Line-Replaceable Unit (LRU) design is applied to
reducer, motor, encoder and limit device, azimuth cable wrap, and elevation lock device. Not only for ease of replacement and maintenance, but also suitable for batch production.
4. Concept Design(2) Structure Design
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ITEM WEIGHT (aluminum, Kg) WEIGHT (carbon fibre, Kg)
Reflector 7250 7050
Mount 11250 11250
Total weight 18500 18300
Weight of Dish
4. Concept Design(2) Structure Design
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Structural Mechanics Analysis
EL=10° EL=90°
Finite Element Model
4. Concept Design(2) Structure Design
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Reflector Surface Deformation by Gravity
Structural Mechanics Analysis
EL=10° EL=90°
Best Fit Surface Error by Gravity
4. Concept Design(2) Structure Design
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Less than 1.1 mm
from 15 to 90 degree
Reflector Surface Deformation by Gravity
Structural Mechanics Analysis
4. Concept Design(2) Structure Design
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Reflector Surface Deformation by Wind
Structural Mechanics Analysis
EL=10°
EL=90°
4. Concept Design(2) Structure Design
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Reflector Surface Deformation by Temperature
Structural Mechanics Analysis
Temperature Difference 2°C 5°C 7°C
Surface Error (r.m.s. mm) 0.081 0.203 0.284
4. Concept Design(2) Structure Design
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Strength Analysis
Elevation(degree)
Wind speed (m/s) Gravity Max. stress
(MPa)Safety
coefficient
10° 20 √ 77.4 4.5
54° 20 √ 80.3 4.3
90° 20 √ 150 2.3
54° 45 √ 150 2.3
Structural Mechanics Analysis
4. Concept Design(2) Structure Design
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Antenna Modal Analysis
Order 1 2 3 4 5Resonant
frequency (Hz) 2.42 3.25 4.61 4. 82 4.89
Structural Mechanics Analysis
4. Concept Design(2) Structure Design
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The analysis results show that the structural
performance of antenna can meet the SKA
requirements
Conclusion
Structural Mechanics Analysis
4. Concept Design(2) Structure Design
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Investigation of Main Reflector Types
Carbon Fibre Sandwich Structure(82.5mm thick, 1.5mm/80mm/1mm)
Aluminum Sandwich Structure(83mm thick, 2mm/80mm/1mm)
Deformation of Aluminum Structure Deformation of Carbon Fibre Structure
4. Concept Design(2) Structure Design
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Investigation of Main Reflector Types
Type NameTotal
thickness (mm)
Weight(t)
Maximum Deformation
(mm)
Surface Error
(rms,mm)
1Aluminum sandwich structure
83 2.1 31.5 3.877
2Carbon fibre
sandwich structure
82.5 1.9 22.4 1.629
Surface accuracy of type 2 is better than that of type 1
4. Concept Design(2) Structure Design
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Antenna control unit (ACU)Feed ControlAntenna driversMotorsPower distribution devicesEncodersLocal control pendantLimit and safety protection
device
4. Concept Design(3) Servo Control Design
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Mature ProductState-of-the-art componentsFully digital control systemVery high reliabilityModular design, easy for maintenanceBrushless motors, no maintenanceSpare part available
Main features of control system
4. Concept Design(3) Servo Control Design
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STANDBYPower-on default operation mode or return-on-fault mode
PRESETMoving to predefined position
RATE Moving at user-defined constant velocity
PROGRAM TRACK Tracking of an object along a pre-defined path
STOW Automatically rotating to preset stow position and locking stow pin
4. Concept Design(3) Servo Control Design
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(1) Full Radiation Pattern Calculation5. Main Specification Budget
-180 -135 -90 -45 0 45 90 135 180-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-180 -135 -90 -45 0 45 90 135 180-90
-75
-60
-45
-30
-15
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-150 -100 -50 0 50 100 150-100
-80
-60
-40
-20
0
Angle [dB]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-180 -135 -90 -45 0 45 90 135 180-120
-100
-80
-60
-40
-20
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
f=0.3GHz f=1.5GHz
f=6.0GHz f=10GHz
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First sidelobe: less than -19.73dB
5. Main Specification Budget
First sidelobe (dB)Frequency(GHz) 0° plane 90° plane
0.3 (-22.77, -21.87) (-25.51, -25.51)
1.5 (-21.22, -20.38) (-24.37, -24.37)
6 (-21.21, -20.13) (-24.64, -24.64)
10 (-21.35, -19.73) (-24.24, -24.24)
(1) Full Radiation Pattern Calculation
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Antenna aperture efficiency: more than 59%
Frequency(GHz) η1 η2 η3 η4 η5 η(%)
0.3 0.71 1 0.95 0.98 66
0.9 0.76 1 0.95 0.98 71
1.5(feed 1) 0.78 0.99 0.95 0.98 72
1.5(feed 2) 0.77 0.99 0.95 0.98 71
6 0.81 0.91 0.95 0.98 69
10 0.81 0.78 0.95 0.98 59
5. Main Specification Budget(2) Antenna Aperture Efficiency
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5. Main Specification Budget(3) Noise temperature
0 10 20 30 40 50 60 70 80 9050
55
60
65
70
75
80
85
90
95
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 900
10
20
30
40
50
60
70
80
90
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 900
10
20
30
40
50
60
70
80
90
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 9020
30
40
50
60
70
80
90
100
110
120
130
140
150
Elevation [deg]
Noi
se T
empe
ratu
re [K
]f=10GHz
f=0.3GHz
f=6.0GHz
f=1.5GHz
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5. Main Specification Budget(4) Pointing accuracy
Error source (r.m.s.) Error (arcsec) Residualerror (arcsec)
Modificationmethod
Verticality of the azimuth axis 10 3 Pointing modelAzimuth-Elevation non-
orthogonality 3 3 -
Azimuth bearing run-out 4 4 -Adjust error of sub-reflector
and feed 3 3 -
Gravity deformation 11 2 Lookup table
Thermal deformation <1 <1
Wind deformation - -
Servo error 5 5
Uncertain error 3 3
Total error (RMS) 8.7 arcsec (at night and windless)
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DVAC CONCEPT DESCRIPTION:
PRIME FOCUS DISH — DVAC-2
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Antenna Type Prime Focus Antenna, Diameter 15mFocal length / Diameter ratio (f/D) 0.4
Mount Type AZ-EL-POL mount (AZ, POL:Gear,EL: Screw)
Frequency Band 0.3GHz ~ 10GHz
Frequency Band Switch Manner Switching Feeds within 30s
Surface Accuracy of Main Reflector ≤1.1 mm RMS (at night, under low wind)TBC(at daytime, with wind)
Pointing Accuracy≤10 arcsec RMS (at night and no wind)TBC (at daytime, with wind)
Antenna Aperture Efficiency (%) ≥ 50%First Sidelobe Level ≤-20dB
6. DVAC-2 Specifications
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Polarization Dual-LP/Dual-CP Travel Range AZ:±270°, EL:15°∼ 85°Slew Rates (Max) AZ:3°/s, El:1°/sAcceleration (Max) AZ:3°/s2, El:1°/s2
Wind Velocity Drive to stow :70 km/hSurvival: 160 km/h (at El=90°)
Design Lifetime ≥ 30 years
6. DVAC-2 Specifications
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7. DVAC-2 Concept DesignMain Attractions of DVAC-2 Design
Wide Band Feed (WBF)
Integrated Modular Design
Integrated Main Reflector Surface (Single Panel)
Sealed and Lubricated Driving Devices
Mature Technology
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Design and Manufacture
7. DVAC-2 Concept Design
Feed Control
EL-Driver, Encoder and
Limit &Safety Switches
AZ-Driver, Encoder and
Limit &Safety
Switches
ACU
Remote Computer
Local Control Pendant
P-Driver, Encoder and
Limit &Safety
Switches
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(1) Microwave Optical Design
(2) Structure Design
(3) Servo Control Design
7. DVAC-2 Concept Design
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7. DVAC-2 Concept Design(1) Microwave Optical Design
Feed Design
Main Curve Design
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Main Curve Design F/D =0.4 64°Opening Angle-13dB Feed Edge Taper
7. DVAC-2 Concept Design(1) Microwave Optical Design
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7. DVAC-2 Concept Design(2) Microwave Optical Design
-40 -30 -20 -10 0 10 20 30 40-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-10 -8 -6 -4 -2 0 2 4 6 8 10-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-5 -4 -3 -2 -1 0 1 2 3 4 5-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-3 -2 -1 0 1 2 3-80
-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
f=0.3GHz f=1.5GHz
f=6.0GHz f=10GHz
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Old Design
New DesignSingle PanelSimple StructureLight WeightLow CostFast Installation
7. DVAC-2 Concept Design(2) Structure Design
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Reflector Design
Mount Design
7. DVAC-2 Concept Design(2) Structure Design
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Single integrated main reflector
Minimal spar structure
Turning head design with a lead screw elevation actuator
Four support legs and interchange mechanism for a PAF and 3 SPFs or 2 WBSPFs.
7. DVAC-2 Concept Design(2) Structure Design
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Reflector Design
Main reflector
Back structure
Feed switch mechanism
7. DVAC-2 Concept Design(2) Structure Design
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Reflector Design — Main reflectorDesign 1: Aluminum sandwich structureSingle aluminium panelSkins: 2mm (upper)/1mm (lower) in thickness, 2m in widthSkin and ribs are glued through negative pressure method on mould Surface accuracyσ≤0.8mm
Rib Configuration
7. DVAC-2 Concept Design(2) Structure Design
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Reflector Design — Main reflector
Design 2: Carbon fibre sandwich structureSingle carbon fibre panelCarbon fibre skins: 1.5mm (top)/1mm (bottom) in thickness
Polyurethane foam: in the middle
Surface accuracyσ≤0.8mm
7. DVAC-2 Concept Design(2) Structure Design
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Reflector Design — Back structure
7. DVAC-2 Concept Design(2) Structure Design
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Elevation Part
Azimuth Part
Pedestal
Mount Design
7. DVAC-2 Concept Design(2) Structure Design
8413
6103
Polarization Part
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Mount Design — Azimuth part
Dual-motor anti-backlash driveExternal gear bearing, easy to
maintainSeal cover is used to exclude
dust and sand
7. DVAC-2 Concept Design(2) Structure Design
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Mount Design — Elevation and polarization part
Elevation part: a planetary reducer with a ball screw drivePolarization part: a disc bearing
7. DVAC-2 Concept Design(2) Structure Design
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Mount Design
A flexible-axis drive technique is adopted for Az and EI encoder mechanism.
A double-layer ring structure is used for AZ cable wrap.A modular design for all rotating parts.A Line-Replaceable Unit (LRU) design is applied to
reducer, motor, encoder and limit device, azimuth cable wrap, and elevation lock device. Not only for ease of replacement and maintenance, but also suitable for batch production.
7. DVAC-2 Concept Design(2) Structure Design
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ITEM WEIGHT (aluminum, Kg) WEIGHT (carbon fibre, Kg)
Reflector 6800 6550
Mount 12500 12500
Total weight 19300 19050
Weight of Dish
7. DVAC-2 Concept Design(2) Structure Design
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Antenna control unit (ACU)Feed ControlAntenna driversMotorsPower distribution devicesEncodersLocal control pendantLimit and safety protection
device
7. DVAC-2 Concept Design(3) Servo Control Design
AZ ADU
Feed System
Mount
RFI -Tight Servo Cabinet
PowerDistribution
POL- Driver
ACU
RemoteComputer
EL Motor
Limit&Safety
Switches
AZ Encoder
EL Encoder
AZ Motor1
AZ Motor 2
POL Motor
AC PowerSupply
EL-Driver
AZ-Driver1
AZ-Driver2
LocalControlPendant
Networks
MotorFeed
ControlSensor
POL Encoder
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Mature ProductState-of-the-art componentsFully digital control systemVery high reliabilityModular design, easy for maintenanceBrushless motors, no maintenanceSpare part available
Main advantages of the control system
7. DVAC-2 Concept Design(3) Servo Control Design
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STANDBYPower-on default operation mode or return-on-fault mode
PRESETMoving to predefined position
RATE Moving at user-defined constant velocity
PROGRAM TRACK Tracking of an object along a pre-defined path
STOW Automatically rotating to a preset stow position and locking stow pin
7. DVAC-2 Concept Design(3) Servo Control Design
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-180 -135 -90 -45 0 45 90 135 180-120
-90
-60
-30
0
Angle [deg]
Rel
ativ
e P
ower
[dB
] phi=0°phi=90°
-180 -135 -90 -45 0 45 90 135 180-120
-90
-60
-30
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-180 -135 -90 -45 0 45 90 135 180-100
-80
-60
-40
-20
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
-180 -135 -90 -45 0 45 90 135 180-70
-60
-50
-40
-30
-20
-10
0
Angle [deg]
Rel
ativ
e P
ower
[dB
]
phi=0°phi=90°
(1) Full Radiation Pattern Calculation8. DVAC-2 Specification Budget
f=0.3GHz
f=6.0GHz
f=1.5GHz
f=10GHz
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First sidelobe: less than -28dB
8. DVAC-2 Specification Budget
First sidelobe (dB)Frequency(GHz) 0° plane 90° plane
0.3 (-28.2, -28.2) (-28.2, -28.2)
1.5 (-28.5, -28.5) (-28.5, -28.5)
6 (-28.7, -28.7) (-28.7, -28.7)
10 (-28.9, -28.9) (-28.9, -28.9)
(1) Full Radiation Pattern Calculation
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Antenna aperture efficiency: more than 50%
Frequency(GHz) η1 η2 η3 η4 η5 η(%)
0.3 0.74 1 0.95 0.98 69
0.9 0.71 1 0.95 0.98 66
1.5(feed 1) 0.70 1 0.95 0.98 65
1.5(feed 2) 0.72 1 0.95 0.98 67
6 0.70 0.93 0.95 0.98 60
10 0.68 0.81 0.95 0.98 51
8. DVAC-2 Specification Budget(2) Antenna Aperture Efficiency
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0 10 20 30 40 50 60 70 80 9030
40
50
60
70
80
90
100
110
120
130
140
150
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 900
10
20
30
40
50
60
70
80
90
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 900
10
20
30
40
50
60
70
80
90
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
0 10 20 30 40 50 60 70 80 9050
55
60
65
70
75
80
85
90
95
100
Elevation [deg]
Noi
se T
empe
ratu
re [K
]
f=0.3GHz f=1.5GHz
f=6.0GHz f=10GHz
8. DVAC-2 Specification Budget(3) Noise temperature
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8. DVAC-2 Specification Budget(4) Pointing accuracy
Error source(r.m.s.) Error(arcsec) Residual
error(arcsec)Modification
methodVerticality of the
azimuth axis 10 3 Pointing model
Azimuth-Elevation non-orthogonality 3 3 -
Polarisation-Elevation non-orthogonality 3 3
Azimuth bearing run-out 4 4 -Adjust error of feed 3 3 -Gravity deformation 9 2 Lookup table
Thermal deformation <1 <1
Wind deformation - -
Servo error 5 5
Uncertain error 3 3Total error(RMS) 9.2arcsec(at night and windless)
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Thank YouEND