Research Article

Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach

Table 6

Tracking errors of the AORED with different orders and sampling interval.

Orders of AOREDThird orderFifth order

Sample period
First-order differential error 0.01NegligibleNegligible
Second-order differential error 1.50.02Negligible
Third-order differential error 702.50.0005