TY - JOUR
T1 - Real-time vision-based relative aircraft navigation
AU - Johnson, Eric N.
AU - Calise, Anthony J.
AU - Watanabe, Yoko
AU - Ha, Jincheol
AU - Neidhoefer, James C.
N1 - Funding Information:
This work was supported in part by AFOSR MURI, #F49620-03-1-0401 as well as grants from NSF, AFOSR, ARO, MRI-HEL, and an STTR through Georgia Tech. We also acknowledge Allen Tannenbaum who contributed to the development of the image processing algorithms.
PY - 2007/4
Y1 - 2007/4
N2 - This paper describes two vision-based techniques for the navigation of an aircraft relative to an airborne target using only information from a single camera fixed to the aircraft. These techniques are motivated by problems such as "see and avoid", pursuit, formation flying, and in-air refueling. By applying an Extended Kalman Filter for relative state estimation, both the velocity and position of the aircraft relative to the target can be estimated. While relative states such as bearing can be estimated fairly easily, estimating the range to the target is more difficult because it requires achieving valid depth perception with a single camera. The two techniques presented here offer distinct solutions to this problem. The first technique, Center Only Relative State Estimation, uses optimal control to generate an optimal (sinusoidal) trajectory to a desired location relative to the target that results in accurate range-to-target estimates while making minimal demands on the image processing system. The second technique, Subtended Angle Relative State Estimation, uses more rigorous image processing to arrive at a valid range estimate without requiring the aircraft to follow a prescribed path. Simulation results indicate that both methods yield range estimates of comparable accuracy while placing different demands on the aircraft and its systems.
AB - This paper describes two vision-based techniques for the navigation of an aircraft relative to an airborne target using only information from a single camera fixed to the aircraft. These techniques are motivated by problems such as "see and avoid", pursuit, formation flying, and in-air refueling. By applying an Extended Kalman Filter for relative state estimation, both the velocity and position of the aircraft relative to the target can be estimated. While relative states such as bearing can be estimated fairly easily, estimating the range to the target is more difficult because it requires achieving valid depth perception with a single camera. The two techniques presented here offer distinct solutions to this problem. The first technique, Center Only Relative State Estimation, uses optimal control to generate an optimal (sinusoidal) trajectory to a desired location relative to the target that results in accurate range-to-target estimates while making minimal demands on the image processing system. The second technique, Subtended Angle Relative State Estimation, uses more rigorous image processing to arrive at a valid range estimate without requiring the aircraft to follow a prescribed path. Simulation results indicate that both methods yield range estimates of comparable accuracy while placing different demands on the aircraft and its systems.
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U2 - 10.2514/1.23410
DO - 10.2514/1.23410
M3 - Article
AN - SCOPUS:34547935378
SN - 1542-9423
VL - 4
SP - 707
EP - 738
JO - Journal of Aerospace Computing, Information and Communication
JF - Journal of Aerospace Computing, Information and Communication
IS - 4
ER -