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sensitivity analysis
Standard
ECSS-E-ST-60-30C: Satellite attitude and orbit control system (AOCS) requirements (30 August 2013)Definition
identification of the parameters which impact the AOCS performance, and assessment of their individual contribution to this performanceNotes
- NOTE 1 Only the dominating contributors are of interest. These contributors can include: - Noise, bias and misalignment, for the AOCS sensors and actuators - Satellite mass properties - Satellite configuration variation, e.g. solar array position, sensors and actuators configuration - Measurements outages - Environmental conditions - External and internal disturbances
- NOTE 2 The AOCS performance can be for instance: - Pointing accuracy - Duration of a manoeuvre - Fuel consumption
- NOTE 3 The objective is to have an order of magnitude of the contribution, and this can be achieved by analysis, simulation or test.
Relations
- ECSS-E-ST-70-01C — AOCS
- ECSS-S-ST-00-01C — AOCS
- ECSS-Q-ST-70C Rev.2 — AOCS
- ECSS-E-ST-20-06C Rev.1 — AOCS
- ECSS-E-ST-70-41C — AOCS
- ECSS-E-ST-20-08C Rev. 1 — AOCS
- ECSS-E-ST-70-31C — AOCS
- ECSS-E-ST-70C — AOCS
- ECSS-E-ST-70-11C — AOCS
- ECSS-E-ST-50-13C — AOCS
- ECSS-E-ST-60-30C — AOCS
- ECSS-E-ST-35C Rev. 1 — AOCS
- ECSS-E-ST-32C Rev. 1 — AOCS
- ECSS-E-ST-31C — AOCS
- ECSS-E-ST-10C Rev.1 — AOCS
- ECSS-Q-ST-60-14C Rev.1 Corr.1 — identification
- ECSS-E-ST-32-11C — impact
- ECSS-S-ST-00-01C — performance
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