Second Order Attitude References System (Soars)

• Second Order Attitude References System (Soars)
• Specifications
• Standards
• Parts and Materials
• Cabling and Connections -
• Provisions for Maintainability
• Input Electrical Power -
• Gyroscope Bearings -
• Operation
• Accuracies
• True Air Speed Velocity Invalid Discrete - A separate signal shall
• Compensated First Order Operation
• Built-In-Test Equipment Capabilities (BITE)
• Detailed Design Requirements
• Detailed Design Requirements - Continued
• Erection Control - First Order
• Automatic Fast Erection
• DG Mode Performance -
• Slaved Mode Performance
• Power Interruption
• Malfunction Monitoring
• Automatically Monitored Functions
• System Outputs
• Displacement Gyroscope Assembly
• Acceleration Sensors
• Electronic Control Amplifier
• Heading Coupler Action in DG Mode
• Synchronization Angle Modification
• Amplifier Data Processor
• SOARS Controller
• Synchronizer and Heading Set
• Electronic Compensator Unit
• Adjustment Range
• Classification of Tests
• Electromagnetic Interference/Compatibility Test
• Acceptance Tests
• Sampling Tests - Equipments
• Special Test Schedule
• Reconditioning of Tested Equipment
• Preparation For Delivery
• Associated Equipment
• Figure 1. Minimum Acceptable Accelerometer Criteria
• Figure 2. Detected Deflection From Vertical (Degrees) Normal Erection Rate
• Figure 3. Headling Slaving Rate
• Figure 4. Flight Maneuvers Profile
• Figure 5. Flight Maneuver Profile
• Figure 6. Flight Profile
• Figure 7. System Interconnect Wiring
• Figure 8. Displacement Gyro Form Factor
• Figure 9. Electronic Control Amplifier Form Factor
• Figure 10. Soars Controller Form Factor
• Figure 11. Electronic Compensator Form Factor
• Figure 12. Mounting Tray Displacement Gyro Assembly
• Figure 13. Mounting Tray Electronic Control Amplifier
• Standardization Document Improvement Proposal
• Postage and Fees Paid
• Blank Page

Second Order Attitude References System (Soars)

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