Abstract
A new model predictive convex programming is proposed in this paper for state and input constrained vehicle guidance design. The proposed method defines a convex optimization framework considering a flexibly designed cost function subject to inequality constraints and a sensitivity relation between state increments and input corrections. This formulated convex optimization problem can be solved in a computationally efficient manner. Simulation studies of nonlinear missile and aircraft landing guidance problems demonstrate the effectiveness of the proposed approach.
| Original language | English |
|---|---|
| Article number | 8598772 |
| Pages (from-to) | 2487-2500 |
| Number of pages | 14 |
| Journal | IEEE Transactions on Aerospace and Electronic Systems |
| Volume | 55 |
| Issue number | 5 |
| DOIs | |
| State | Published - Oct 2019 |
Keywords
- Aircraft landing
- constrained guidance
- missile guidance
- model predictive convex programming (MPCP)
- terrain constraints