Abstract
The angular glint of aircraft formation was studied for avoiding it to be intercepted. The angular glint of the aircraft formation was modeled as an evenly distributed N-point scattering center, and the linear error of the angular glint and its distribution characteristics were calculated with the phase gradient method. A mathematical model of the apposition between four aircrafts in different formation modes and a typical surface-to-air missile was established. A simulation was performed by the model. The simulated result shows that it is effective to avoid intercepting with reasonable aircraft formation mode.
| Original language | English |
|---|---|
| Pages (from-to) | 1479-1484 |
| Number of pages | 6 |
| Journal | Binggong Xuebao/Acta Armamentarii |
| Volume | 29 |
| Issue number | 12 |
| State | Published - Dec 2008 |
Keywords
- Aircraft
- Angular glint
- Extend target
- Formation
- Phase gradient
- Radar engineering