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First published online November 24, 2003
Journal of Experimental Biology 207, 133-142 (2004)
Published by The Company of Biologists 2004
doi: 10.1242/jeb.00731
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Summation of visual and mechanosensory feedback in Drosophila flight control

Alana Sherman1 and Michael H. Dickinson2,*

1 UCB/UCSF Joint Bioengineering Graduate Group, University of California, Berkeley, CA 94720, USA
2 Bioengineering, California Institute of Technology, Pasadena, CA 91125, USA



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Fig. 1. (A) Cartoon of fly showing the compound eyes and mechanosensory halteres. (B) The flight simulator, which delivers visual and mechanosensory stimuli, is composed of a wrap-around light-emitting diode (LED) display mounted within a 3 degrees-of-freedom rotational gimbal. The fly is mounted in the center of the display, above a sensor that measures the left and right wingbeat amplitudes. (C) Moving striped patterns simulate the optic flow generated when the fly rotates along the roll and pitch axes.

 


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Fig. 2. Flies respond to mechanical, visual and concurrent oscillations with sinusoidal modulations of wingbeat amplitude. Rotational stimuli were applied around the roll axis. Each trace represents the time-averaged response to six trials for a single fly. (A) Concurrent visual and mechanical oscillations phase shifted by 180° elicit strong responses (Rm+v) that are approximately equal to the sum of the responses to each stimuli presented separately (Rm+Rv). (B) When visual and mechanical stimuli are presented with a 0° phase offset, flies display almost no response. (C) At a 270° phase offset, responses are intermediate in amplitude. L, left; R, right; {varphi}, phase offset; {theta}, position. Wingbeat amplitude (WBA) is plotted in normalized units.

 


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Fig. 3. The magnitude of the wingbeat responses to concurrent oscillations about the pitch (A) and roll (B) axes is a function of the phase offset between mechanical and visual stimuli. (A) Pitch axis responses (mean ± S.E.M., N=10 flies). (B) Roll axis responses (mean ± S.E.M., N=14 flies). The amplitude of the sine fits to wingbeat data (Rm+v; green circles) are plotted against phase offset ({varphi}). In addition, two possible fits for the data are plotted: linear summation (Rm+Rv; black curve) and scaled summation ({alpha}RmRv; red curve). The two fitted functions are 4th order polynomials.

 


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Fig. 4. The attenuation of visually elicited motor responses is not a linear function of the magnitude of haltere stimulation. With {alpha} set to 1, the scaling factor ß was calculated for multiple flies during concurrent oscillations in which the amplitude of the visual stimulus was fixed at 30° and the amplitude of the mechanical stimulus (u) was varied. (A) ß (mean ± S.E.M.) versus u for three phase relationships ({varphi}): 180°, 270° and 90° (N=8, 9 and 9 flies, respectively). (B) Amplitude of sine fit to time-averaged wingbeat responses versus u for {varphi}=180°, 270° and 90° (N=8, 9 and 9, respectively). Data fit by weighted sum (spline approximation of the fit), {alpha}RmRv, with {alpha}=1.17 and ß=0.65.

 


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Fig. 5. Responses to mechanical and visual oscillations about orthogonal axes have both a pitch and roll component. (A) The wingbeat response to mechanical pitch (Rm), visual roll (Rv) and the two stimuli concurrently (Rm+v) of a single fly. Each trace represents the time-averaged response to 21 trials of each stimulus. (B) Magnitude of roll and pitch components in response to simultaneous visual roll and mechanical pitch (mean ± S.E.M., N=10 flies). (C) Responses to visual pitch and mechanical roll (mean ± S.E.M., N=13 flies). The y-axis represents normalized wingbeat amplitude ({Delta}WBA) units.

 


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Fig. 6. Input from the halteres and visual system are combined in a weighted sum by the flight control system. The weighting of the visual feedback is dependent on the presence of haltere input but appears to be constant over a wide range of haltere stimulation. The processing of each sensory input is represented by a transfer function based on our previous frequency response analysis. G, gain; {omega}, angular velocity.

 

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© The Company of Biologists Ltd 2004