Integration Tests. Subsequent to successful completion of installation and integration the successful bidder shall perform end-to- end integration tests, functional tests, and safety features verification. The successful bidder shall ensure that the tests are performed as per the approved plan and procedures. The integration testing shall be carried out by the successful bidder at the installation site with the participation of MCF representatives. The test procedures and the results will be reviewed and validated by purchaser.
Integration Tests. Additional work has been realized for providing a Continuous Integration / Continuous Development (CI/CD) system allowing executing integration tests on top of the federated testbed. This CI/CD system allows testing realistic use cases of all the components of the SoftFIRE Middleware on an automated way. Xxxxxxx [10] is used for the automation of the tests. Every night a Xxxxxxx job runs a comprehensive test. The test is a separate project which exists only for the purpose of testing the SoftFIRE middleware. The test executes a comprehensive scenario on different testbeds utilizing every type of resource in an experiment. These are the steps of the integration test:
1. Creation of a new experimenter
2. Upload of an experiment making use of all the available resources
3. Deployment of the experiment
4. Validation of the deployed experiment 5. Removal of the experiment
Integration Tests. 4-14 4.3.2 Initial Reference Performance Test.........................................................4-14 4.3.3 Thermal Balance/Thermal Vacuum Test........................................................4-16 4.3.4 Spacecraft Alignments......................................................................4-20 4.3.5 Sinusoidal Vibration.......................................................................4-20 4.3.6 Acoustic Vibration Test....................................................................4-21 4.3.7 Shock and Deployment Tests.................................................................4-21 4.3.8 Spacecraft Mass Properties Measurements....................................................4-21 4.3.9 Final Performance Testing..................................................................4-22 4.3.10 RF Range Test.............................................................................4-22 4.3.11 Electro Magnetic Compatibility (EMC) Test.................................................4-23 5 --FLIGHT ACCEPTANCE TESTS.........................................................................................5-1 5.1 UNIT ACCEPTANCE TESTS..................................................................................5-1 5.1.1 Power Handling and Passive Intermodulation (PIM)............................................5-2 5.1.2 Traveling Wave Tube Amplifiers Burn-In......................................................5-2 5.2 SUBSYSTEM ACCEPTANCE TESTS............................................................................5-3 5.2.1
Integration Tests. Information to support integration testing is provided in deliverable D2.5. Per Technical component following information is provided: Business Case Master Test Plan Services Functional Test Plan Cases and scripts Unit Test Cases Infrastructure Unit Test Cases
Integration Tests. This section documents all actions related to planning and executing tests of the language tools integrated into ATLAS platform.
