| contributor author | Wen Qiuqiu | |
| contributor author | Xia Qunli | |
| contributor author | Su Weixia | |
| date accessioned | 2017-12-16T09:22:50Z | |
| date available | 2017-12-16T09:22:50Z | |
| date issued | 2016 | |
| identifier other | %28ASCE%29AS.1943-5525.0000552.pdf | |
| identifier uri | http://138.201.223.254:8080/yetl1/handle/yetl/4242122 | |
| description abstract | To avoid the mathematical singularity of polar converting in bank-to-turn (BTT) guidance and to provide the specified terminal impact angle, a BTT guidance law with impact-angle constraint (BTT-GL/IA) is presented. Considering the influence of the impact-angle control and target maneuver to the miss-distance, a new form zero-effort miss-distance with impact angle (ZEM/IA) is introduced. Referring to the Lyapunov-like approach used to drive the guidance law in the prior literature, a Lyapunov function is constructed in terms of ZEM/IA. Based on the Lyapunov stability theorem, a negative definite function is designed, and the BTT-GL/IA is derived. Next, BTT-GL/IA is implemented in another form with the variables as the line-of-sight angle and its rate, which are easily measured by the seeker. When using BTT-GL/IA, the guidance law tends to maintain smooth and continuously-varied body acceleration and roll-angle commands while satisfying the impact position and angle constraints. The problem of a mathematical singularity in normal BTT polar converting logic is avoided. Finally, both the maneuverable and stationary targets with different impact-angle constraints are considered in numerical simulations. Through various simulation results, the effectiveness and practicality of the BTT-GL/IA are demonstrated. | |
| publisher | American Society of Civil Engineers | |
| title | Bank-to-Turn Guidance Law with Terminal Impact-Angle Constraint | |
| type | Journal Paper | |
| journal volume | 29 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000552 | |
| tree | Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 003 | |
| contenttype | Fulltext | |