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FSW Test 001 (next)


Test 001: "1553 Interface Test"

This test shall first verify the electrical characteristics of the LAT 1553 interface, then demonstrate (in conjunction with a spacecraft simulator) that the LAT can exist on the bus without responding to messages directed to other remote terminals. Next, processing of telemetry requests shall be demonstrated, followed by exercising the command interface to the LAT and verifying that all commands and command data are correctly interpreted. Commands need not be executed to successfully carry out this test. Timing measurements for the standard message traffic shall also be performed.

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Section Description Other Tests
5.2 Hardware Interfaces
5.2.2 Hardware Interfaces with the Spacecraft
5.2.2.1 Command, Telemetry, and Data Bus (CTDB)
5.2.2.1.1 Command, Telemetry, and Data Bus Protocol - SC
5.2.2.1.2 Command Rates 002a
5.2.2.1.3 Data Format
5.3 Functional Requirements
5.3.1 Boot
5.3.2 Watchdog 009b
5.3.3 Command Processing
5.3.3.1 SC Command Processing by SIU 002a
5.3.3.2 Command Execution Notification 002a
5.3.3.3 Command Completion Status 002a
5.3.3.4 Command Dispatch 002a
5.3.3.5 Command Format
5.3.3.6 Command Execution 002a
5.3.3.7 Command Execution Sequence 002a
5.3.3.8 Multiple Block Commands 002a
5.3.3.9 Command Validation
5.3.4 Time Services
5.3.5 Telemetry
5.3.6 Deadtime Management
5.3.7 File and Memory Management
5.3.8 Event Monitoring and Delivery
5.3.9 Event Filtering
5.3.10 GRB Detection
5.3.11 GRB Response
5.3.12 Charge Injection Calibration
5.3.13 Diagnostics
5.3.14 Ancillary Data from SC
5.3.14.1 SSR Usage
5.3.14.2 LAT In or Out of SAA 013a
5.3.14.3 GPS Status
5.3.14.4 Transmitter Status
5.3.15 Mode Control 013a, 013b
5.3.16 Safety
5.3.17 Configuration
5.3.18 SAA Transit
5.3.19 Thermal Control System (TCS)