Exam2 Review2
Exam 2 Review: UAS, GNSS, and Photogrammetry
1. Introduction to UAS
Overview of Unmanned Aerial Systems (UAS) and their importance in various fields including surveying and mapping.
2. Global Navigation Satellite Systems (GNSS)
Key GNSS Systems:
GPS (U.S.A.)
GLONASS (Russia)
GALILEO (EU)
Provides low and high precision services.
BEIDOU/COMPASS (China)
QUASI-ZENITH SATELLITE SYSTEM (QZSS - Japan)
IRNSS (India)
3. NAVSTAR GPS
Development History:
1970s: Early GPS experiments; civilian use started in the 1980s.
Initially for military purposes; now globally used.
System Characteristics:
Passive system; no limits on the number of receivers.
Composed of three segments: space, control, user.
Operates in a large bandwidth for transmitting vast amounts of data.
4. GPS Satellite Constellation
Consists of 24 satellites plus spares positioned across six orbital planes.
Inclinations provide maximum global coverage.
5. Dilution of Precision (DOP)
Concept of DOP:
Indicates the geometrical strength of satellite configuration above the observer.
Types include:
Horizontal DOP (HDOP)
Vertical DOP (VDOP)
Position DOP (PDOP) = HDOP + VDOP
A PDOP value of 6 or less is optimal.
Outages occur when DOP exceeds acceptable limits.
6. Good vs. Bad DOP
Bad DOP:
Satellites clustered in one area leads to high DOP values.
Good DOP:
Satellites spread across the sky resulting in low DOP values.
7. Broadcast Ephemeris
Provides satellite positions relative to Earth.
While pre-calculated, it lacks precision compared to precise ephemeris data.
8. Error Budget
Key factors contributing to GPS accuracy:
Satellite clock bias
Ionospheric effects
Tropospheric effects
Orbital bias
Receiver noise
Multipath interference
9. Multipath Errors
Definition:
Reception of GPS signals via multiple indirect paths.
Reflected signals are weaker due to their diffused nature.
10. Antenna Design for Multipath Reduction
Key Designs:
Ground Plane: Eliminates low-angle signals.
Choke Ring Design: Reduces low elevation gain.
Recommended cutoff angle of 15°.
11. Real-Time Kinematic (RTK)
Accuracy of +/- 2 cm achieved through:
Using a carrier phase radio connection from base station(s) to rovers.
Developed in 1980s for real-time positional accuracy over distances of 10-20 km.
12. CORS (Continuously Operating Reference Stations)
Offer relative positioning without the need for a personal base station.
Support DGPS and RTK using dual-frequency GPS data formatted in RINEX.
13. RTK and DGPS
Corrections from base stations are applied to rover data, relying on correlated errors over shorter baselines.
14. GNSS Applications
Key Sectors:
Agriculture: Field mapping, soil sampling.
Aviation: Navigation and tracking.
Construction: Machine control.
Environment: Wildlife studies, forest management.
Marine: Vessel control, waterway management.
Public Safety: Monitoring and emergency services.
Transportation: Fleet tracking, intelligent systems.
Recreation: Hikers, cyclists.
Surveying and mapping.
15. Stereo Perception
Humans perceive depth based on the parallactic angle formed by the intersection of lines of sight.
16. Stereo Aerial Photos
Vertical images from two locations (A and B).
Height of buildings can be deduced from depth cues and parallactic angles.
17. Multi-ray Photogrammetry
Involves two or more cameras to reduce error.
18. Pix4D Approach
Software utilizing automation to enhance image processing through high redundancy.
19. Automatic Tie Points
Unique features detected and matched across images to establish reference points for alignment.
20. Image Content and Quality
Ideal Conditions:
Heterogeneous, non-reflective, static scenes with simple geometry.
Not Recommended:
Homogeneous, reflective, dynamic scenes with complex geometry.
21. Stereoscopic Parallax
Apparent displacement caused by a change in observation position; demonstrated in hand-held visual observations.
22. Flight-line Axes for Stereoscopic Measurement
Measure coordinates from stereo images to determine feature positions.
23. Overlapping Aerial Photographs
Importance of side and end lap in overlapping images for accurate measurements.
24. Image Acquisition Techniques
Recommended flight paths include 75% end lap and 70% side lap with nadir camera orientation.
25. UAS Critical Camera Features
Features include:
Computer controllable, high resolution, stability in flight, easy file extraction.
26. UAS Overview
Flexibility in image acquisition with higher overlaps compared to conventional methods.
27. Multirotor vs. Fixed Wing UAS
Multirotor Advantages:
Maneuverability, lower price, compact, higher payload capacity.
Fixed Wing Advantages:
Stability in wind, longer range, safer recovery.
28. Summary Comparison Table
Comparison of UAS types based on maneuverability, price, size, and other key features.
29. 2D, 3D, & 4D from UAS
Visual Outputs:
2D: Orthophoto
3D: Digital Surface Model
4D: Change detection over time.
30. Quality – Project Dependency
Factors affecting quality include terrain, weather, equipment, and planning strategies.
31. Quality – Accuracy
Relative vs. Absolute Accuracy:
Relative: Based on GPS.
Absolute: Incorporates Ground Control Points (GCPs) for verification.
32. Ground Control Point (GCP)
Characteristics of GCPs:
Static, flat, matte finish, and contrasting appearance.
33. GCP Placement Recommendations
Recommended number of GCPs for modeling and verification. Spacing considerations.
34. UAS Applications
Extensive applications including:
Search and rescue, surveying, environmental studies, marketing, and more.