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Satellite Construction Attitude Control and Determination System Attitude Control and Determination System Jan Hales, Martin Pedersen & Klaus Krogsgaard
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2 ACDS Concept Magnetometer and magnetotorquers Sun sensor for unambiguous determination B-dot control Optional: full three-axis control Magnetometer and magnetotorquers Sun sensor for unambiguous determination B-dot control Optional: full three-axis control
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3 Sun Sensor Linear analog slit sensor (MOEMS) –FOV: 70° (Required: 54.75°) –Theoretical resolution:0.07° (Required: 1°) –Chip size:8100µm 6900µm –Expected mass: 2.5-3g –Expected size (PCB):25mm 35mm Linear analog slit sensor (MOEMS) –FOV: 70° (Required: 54.75°) –Theoretical resolution:0.07° (Required: 1°) –Chip size:8100µm 6900µm –Expected mass: 2.5-3g –Expected size (PCB):25mm 35mm
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4 Sun Sensor – Reflection
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5 Sun Sensor – Linear, how? Independent of: –Degradation –Temperature –Dark currents –Cosine dependence –Sun power fluctuations –Albedo intensity contributions Independent of: –Degradation –Temperature –Dark currents –Cosine dependence –Sun power fluctuations –Albedo intensity contributions Division implemented using Vref of an ADC Reference area used to cancel out various dependencies
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6 I t1 I t2 Sun Sensor – Linear It It I t
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7 I t /I ref I ref It It Sun Sensor – Linear I t /I ref
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8 Sun Sensor – Circuit
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9 Sun Sensor Chip Conservative mask design Digital sensor chip with 70° FOV and 0.6° resolution Process sequence compatible with MIC’s cleanroom
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10 Magnetometer Specification: –Range: |B| [18200nT;49800nT] –Accuracy: < 1º sin(1º)·18200nT=300nT –Resolution:> 8.4-bit effective Design goals: –Range:± 64000nT –Accuracy:< 50nT –Sample time:< 2ms per axis Specification: –Range: |B| [18200nT;49800nT] –Accuracy: < 1º sin(1º)·18200nT=300nT –Resolution:> 8.4-bit effective Design goals: –Range:± 64000nT –Accuracy:< 50nT –Sample time:< 2ms per axis
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11 Magnetoresistive sensor Sensor –Honeywell HMC1021: Wheatstone bridge with intergrated offset and reset coils Sensor –Honeywell HMC1021: Wheatstone bridge with intergrated offset and reset coils Compensation –Constant field, linearity error reduced to noise –Temperature drift: sensor, amplifier, A/D converter, and voltager reference Compensation –Constant field, linearity error reduced to noise –Temperature drift: sensor, amplifier, A/D converter, and voltager reference
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12 Magnetotorquers Torque 0.6 – 1.5 Nm H-brige configuration as driver circuit. Switch frequency: f = 32kHz Switch frequency: f = 32kHz
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13 Environment Modeling Environment models: –Orbit (SGP) –Geomagnetic (IGRF2000) Environment models: –Orbit (SGP) –Geomagnetic (IGRF2000) – Sun positioning – Gravity Gradient
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