21-03-2011, 09:25 AM
Submitted by
Ajesh.M.L
[attachment=10619]
Introduction
Objectives
1. Find 6 DOF estimation
2. Find Robust Navigation Solution
Consist of PSD & DSP
Limitations of GPS
1. Less Precision
2. Complex infrastructure
3. Low accuracy
Sensor Description
Activated by energy from beacons
Generates electrical current in 4 directions
Current imbalances are linearly proportional to location of image centroid
Factors affecting measurement
Short wavelength light from sun & other discharge light act as beacons
High power beacon signal saturate output of preamplifier
Preventive Measures
Optical filter to block visible light.
Modulate beacon current with high frequency.
Feed back loop to control the beacon intensity.
VISNAV Block Diagram
Signal Processing
• Sinusoidal carrier of 40kHz frequency applied to modulate each drive current from the four terminals of the PSD.
• The output of the PSD is applied to the preamplifier
• The signal is converted into digital form through an analog to digital converter.
• The digital data fed into the two DSP’s from this we get a sensor coordinates.
• Beacon control data is communicated to BCM.
• Control data is FSK modulated
• Data then transmitted via wireless page link to control amplitude of beacons.
• This closed loop system estimates 6 DOF of sensor.
DSP Implementation
Functions of DSP TMS320C55X-act as demodulator
Functions of DSP TMS320VC33 act as 6 DOF estimator
ADVANTAGES
Reprogrammable
Insensitive to temperature variation and ageing effect
Wide field of view
Very small and compact size
Number can be increased upto 16 beacons
DISADVANTAGE
The signal may be blocked by the opaque objects in their path
Applications
1. Autonomous aerial refuelling.
• Aerial Refuelling
Requires light sources on the refuelling target frame
optical sensor on the aircraft frame.
Can be used even in 100% cloud cover,total darkness and adverse condition
2. Spacecraft Docking
Beacons & beacon contoller on target spacecraft & sensor on chasing space craft
VISNAV enables docking simple and easy
Conclusions
100 Hz update rate 6DOF data possible with small low power sensor/beacons to 100+m.
Beacon signal modulation and optical filtering
Excellent ambient light rejection.
Realtime beacon selection/intensity control
Minimize power requirements.
Very wide field of view, no moving parts.
Distributed beacons
Very large operating space
Ajesh.M.L
[attachment=10619]
Introduction
Objectives
1. Find 6 DOF estimation
2. Find Robust Navigation Solution
Consist of PSD & DSP
Limitations of GPS
1. Less Precision
2. Complex infrastructure
3. Low accuracy
Sensor Description
Activated by energy from beacons
Generates electrical current in 4 directions
Current imbalances are linearly proportional to location of image centroid
Factors affecting measurement
Short wavelength light from sun & other discharge light act as beacons
High power beacon signal saturate output of preamplifier
Preventive Measures
Optical filter to block visible light.
Modulate beacon current with high frequency.
Feed back loop to control the beacon intensity.
VISNAV Block Diagram
Signal Processing
• Sinusoidal carrier of 40kHz frequency applied to modulate each drive current from the four terminals of the PSD.
• The output of the PSD is applied to the preamplifier
• The signal is converted into digital form through an analog to digital converter.
• The digital data fed into the two DSP’s from this we get a sensor coordinates.
• Beacon control data is communicated to BCM.
• Control data is FSK modulated
• Data then transmitted via wireless page link to control amplitude of beacons.
• This closed loop system estimates 6 DOF of sensor.
DSP Implementation
Functions of DSP TMS320C55X-act as demodulator
Functions of DSP TMS320VC33 act as 6 DOF estimator
ADVANTAGES
Reprogrammable
Insensitive to temperature variation and ageing effect
Wide field of view
Very small and compact size
Number can be increased upto 16 beacons
DISADVANTAGE
The signal may be blocked by the opaque objects in their path
Applications
1. Autonomous aerial refuelling.
• Aerial Refuelling
Requires light sources on the refuelling target frame
optical sensor on the aircraft frame.
Can be used even in 100% cloud cover,total darkness and adverse condition
2. Spacecraft Docking
Beacons & beacon contoller on target spacecraft & sensor on chasing space craft
VISNAV enables docking simple and easy
Conclusions
100 Hz update rate 6DOF data possible with small low power sensor/beacons to 100+m.
Beacon signal modulation and optical filtering
Excellent ambient light rejection.
Realtime beacon selection/intensity control
Minimize power requirements.
Very wide field of view, no moving parts.
Distributed beacons
Very large operating space