“Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor,...

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“Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin

Transcript of “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor,...

Page 1: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

“Attitude on a Chip” Single Antenna GPS Attitude

(SAGA)

E. Glenn Lightsey

Associate Professor, Aerospace Engineering

The University of Texas at Austin

Page 2: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

Problem

Autonomous vehicles are undergoing miniaturization• Satellites, unmanned aerial vehicles (UAVs), robotics

Sensors must be available that provide required information• Many sensors are not suited to miniaturization for size, cost,

and complexity reasons

Page 3: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

• A device capable of determining platform attitude pointing to within a few degrees

Based on a GPS receiver, it also provides:• position, time, and relative solutions

Highly suited for vehicle automation

Highly suited for miniaturi-zation (could ultimately fit on a single chip and antenna) current working

prototype< 2” x 2” x 4”

Our invention

Page 4: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

Principle of operation

GPS signal-to-noise ratio (SNR) measurements, when coupled with an external vector sensor, such as a Three-Axis Magnetometer (TAM), can be used to provide coarse attitude determination accurate to within 5˚ to 10˚.

SNR g * (1+cos())

cos() = Â • L

 is the antenna boresight vector

L is the normalized LOS vector to the GPS satellite

is the incident angle of incoming GPS signals, called the antenna off-boresight angle

ˆ

ˆ

Page 5: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

GPS measurement model

A quaternion point rotation can be used to relate the nominal antenna boresight vector with the rotated body-fixed vector:

Ârot = (2q2 – 1) Âk + 2(q • Âk) q + 2q0 (Âk × q)

The SNR measurement model is the cosine of the angle between this rotated antenna boresight vector and the corresponding GPS line-of-sight vector:

G1 = Ârot • L = cos()

Y1 = ƒ(SNR)

ˆ

0

Page 6: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

Three-axis magnetometer (TAM)

Simulated investigation• Truth – 10th order IGRF

2000 model

• Measurements – 6th order IGRF 1995 model plus 0.3mG measurement noise

Spacecraft implementation• Honeywell HMC2003 three-axis magnetic

sensor

• Atmel ATmega128 microcontroller interface circuit

Page 7: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

Testing results

Page 8: “Attitude on a Chip” Single Antenna GPS Attitude (SAGA) E. Glenn Lightsey Associate Professor, Aerospace Engineering The University of Texas at Austin.

Formation Autonomy Spacecraft with Thrust, Relnav, Attitude, and Crosslink

Two student-built nanosatellites delivered to U.S. Air Force Research Labs

Expected launch in 2007

SAGA will fly on two satellites