Attitude Determination and Remote...
Transcript of Attitude Determination and Remote...
AERO4701 Space Engineering 3 – Week8
Attitude Determination and Remote Sensing
AERO4701 Space Engineering 3 – Week 8
AERO4701 Space Engineering 3 – Week8
Course So Far …
• Orbital Mechanics, Perturbations• Global Positioning System• Satellite Attitude Determination• Introduction to Data Fusion
AERO4701 Space Engineering 3 – Week8
Overview
• First Hour– Satellite Pointing and Geo-location– Earth Viewing Geometry– Mapping and Pointing Budgets
AERO4701 Space Engineering 3 – Week8
Remote Sensing
AERO4701 Space Engineering 3 – Week8
Resolution and Swath Width
AERO4701 Space Engineering 3 – Week8
Measures of Coverage
• Percentage coverage –number of times a point is observed
• Maximum Coverage Gap
• Mean Coverage Gap
• Time Average Gap – mean gap / time
• Mean response time –average time from when we receive a random request to observe a point until it is observed
AERO4701 Space Engineering 3 – Week8
Geo-location from remote sensor observations
• Using Radar:
AERO4701 Space Engineering 3 – Week8
Geo-location from remote sensor observations
• Using Camera (can compute by assuming the earth in spherical and finding the intersection of the line of sight and the Earth’s surface):
• Substitute 3 equations into equation for the Earth’s sphere:
AERO4701 Space Engineering 3 – Week8
Geo-location from remote sensor observations
AERO4701 Space Engineering 3 – Week8
Earth Viewing Geometry
AERO4701 Space Engineering 3 – Week8
Single View Coverage
AERO4701 Space Engineering 3 – Week8
Earth Viewing Geometry
AERO4701 Space Engineering 3 – Week8
Earth Viewing Geometry - Example
• Calculate the coverage of a single sensor observation of a nadir pointing sensor with a field of view of 47o from a satellite at an altitude of 800km
• ρ = sin-1(6378/(6378+800)) = 62.6914o
• ε = cos-1(sin(47o/2)/sin(62.6914o)) = 63.3360o
• λ = 90o – ε – η = 3.1640o
AERO4701 Space Engineering 3 – Week8
Earth Viewing Geometry - Example
AERO4701 Space Engineering 3 – Week8
Mapping and Pointing Budgets• Pointing Tasks: instruments towards ground,
communications antenna pointing• Mapping Tasks: climate, atmospheric and ocean
studies, monitoring of bushfires and other natural disasters, surveillance
• We want to determine what sensing, timing and system accuracies are needed to achieve a given mapping or pointing accuracy
AERO4701 Space Engineering 3 – Week8
Error Sources
AERO4701 Space Engineering 3 – Week8
Error Sources
AERO4701 Space Engineering 3 – Week8
Mapping and Pointing Errors
AERO4701 Space Engineering 3 – Week8
Mapping and Pointing Errors
• Attitude Errors and Target Altitude Errors: as ε->0o, errors in mapping becomes large
• Generally larger errors for larger altitude Rs
AERO4701 Space Engineering 3 – Week8
Example Mapping Errors
AERO4701 Space Engineering 3 – Week8
Example Mapping Errors
AERO4701 Space Engineering 3 – Week8
Example Pointing Errors
AERO4701 Space Engineering 3 – Week8
Remote Sensing Mission Design
• Need to balance sensor coverage and accuracy• Coverage effected mainly by orbital parameters (altitude
etc.)• Accuracy effected by positioning and attitude
determination errors but also by orbital parameters• Trade-off between coverage, accuracy, orbit, quality/cost
of attitude determination hardware
• Next week: design case studies looking into the design process for several satellite missions