A. Derivation of the main beam-pointing equation

A linear traveling-wave array of radiating elements with a constant interelement spacing, d, is considered; see Fig. A. The change in phase from a to c is 2π/λ ∙ d cos ϕ where λ is the free space wavelength and ϕ the main beam pointing direction from forward endfire. Similarly, the phase change from a to b is 2π/λg ∙ d; λg is the waveguide wavelength. An additional phase shift of –mπ (m = 0, 1, 2, 3) is introduced with each succeeding element. The value of m depends on how the elements are fed—in or out of phase (m = 1 and m = 3 correspond to staggered slots and m = 0 and m = 2 correspond to collinear or inline slots). Points c and b are in phase yielding.

Solving Eq. 2 for ϕ gives an expression for the main beam pointing direction

For the TE10 mode of the waveguide wavelength, λg, is related to the relative dielectric constant, K, and the inside width, a, of the rectangular waveguide by

The beam pointing direction is, thus

Eq. 5 represents the beam pointing direction for the array factor of an array of omnidirectional elements.

The effective bias toward broadside of the beam pointing direction of traveling-wave arrays is caused by the variation of the magnitude of the element factor from broadside to endfire. Radiation pattern beams of non-broadside arrays are asymmetrical because the magnitude of the element factor is maximum at broadside and decreases toward forward endfire and rear endfire. In particular, the forward endfire (rear endfire) portion of the main lobe of a non-broadside beam is somewhat lower than the corresponding portion of a broadside beam from an array of the same length. Lowering the portion of the main beam closest to forward endfire (rear endfire) with respect to the portion closest to broadside effectively moves the beam peak toward broadside. The wider the beam and the closer it is to forward endfire (rear endfire), the greater the relative reduction of the forward endfire (rear endfire) portion of the main beam and the greater the effective bias toward broadside.

C. Grating lobes

The maximum interelement spacing, dM, of radiating elements in a traveling-wave array (which will not allow gain reducing grating lobes to appear in the radiation pattern) is a function of the angular offset, ϕ0, of the main beam from endfire, as expressed in Eq. 6 for infinitely narrow beamwidths.

where λ is the operating wavelength. A more general expression applicable to arrays of various beamwidths is

where BW10 dB is the 10 dB beamwidth or the angular width of the main beam measured at the 10 dB down points. Figs. 1 through 11 are each plotted with interelement spacings of 0.55λ and 0.65λ which correspond to minimum angular offsets of the main beam from endfire of 34.9 degrees and 57.3 degrees, respectively, (which will not allow grating lobes to appear in the radiation pattern) for infinitely narrow beams. The appropriate portions of the curves have been eliminated due to grating lobes appearing in the radiation pattern as predicted by Eq. 6. The antenna designer should use the more general expression of Eq. 7 to check their particular array for possible grating lobes.

D. Double moding

Eq. 5 was derived for a TE10 mode of propagation in a rectangular waveguide. Under certain conditions the TE20 mode will propagate, and those conditions (waveguide widths allowing TE20 cut off frequencies below the operating frequency) have been eliminated from the curves. The expression for TE20 cut off frequency is

where

c = velocity of light

K = dielectric constant

a = inside width of the rectangular waveguide